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Source: The Open Library

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1Elements of flow and diffusion processes in separation nozzles

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“Elements of flow and diffusion processes in separation nozzles” Metadata:

  • Title: ➤  Elements of flow and diffusion processes in separation nozzles
  • Author:
  • Language: English
  • Number of Pages: Median: 140
  • Publisher: Springer-Verlag
  • Publish Date:
  • Publish Location: Berlin - New York

“Elements of flow and diffusion processes in separation nozzles” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1983
  • Is Full Text Available: Yes
  • Is The Book Public: No
  • Access Status: Borrowable

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2Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles

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“Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles” Metadata:

  • Title: ➤  Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles
  • Author:
  • Language: English
  • Number of Pages: Median: 111
  • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: ➤  Washington, D.C - [Springfield, Va

“Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1979
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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3Two-dimensional converging-diverging rippled nozzles at transonic speeds

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“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:

  • Title: ➤  Two-dimensional converging-diverging rippled nozzles at transonic speeds
  • Author:
  • Language: English
  • Number of Pages: Median: 105
  • Publisher: ➤  Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: ➤  Hampton - Hampton, Va - [Springfield, Va

“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1994
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    4Turbofan forced mixer-nozzle internal flowfield

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    “Turbofan forced mixer-nozzle internal flowfield” Metadata:

    • Title: ➤  Turbofan forced mixer-nozzle internal flowfield
    • Author:
    • Language: English
    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - [Springfield, Va

    “Turbofan forced mixer-nozzle internal flowfield” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1982
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    5High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

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    “High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Metadata:

    • Title: ➤  High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
    • Author:
    • Language: English
    • Number of Pages: Median: 51
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

    “High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1999
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

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      6Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

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      “Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes” Metadata:

      • Title: ➤  Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes
      • Author:
      • Language: English
      • Number of Pages: Median: 77
      • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service - Langley Research Center
      • Publish Date:
      • Publish Location: ➤  Washington, D.C - Hampton, Va - Springfield, Va

      “Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1991
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

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        7Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle

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        “Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle” Metadata:

        • Title: ➤  Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle
        • Author:
        • Language: English
        • Number of Pages: Median: 107
        • Publisher: ➤  National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
        • Publish Date:
        • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

        “Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1993
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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          8Use of Navier-Stokes methods for the calculation of high-speed nozzle flow fields

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          “Use of Navier-Stokes methods for the calculation of high-speed nozzle flow fields” Metadata:

          • Title: ➤  Use of Navier-Stokes methods for the calculation of high-speed nozzle flow fields
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

          “Use of Navier-Stokes methods for the calculation of high-speed nozzle flow fields” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1994
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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            9Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft

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            “Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft” Metadata:

            • Title: ➤  Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft
            • Author:
            • Language: English
            • Number of Pages: Median: 10
            • Publisher: ➤  For sale by the National Technical Information Service - NASA
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

            “Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1990
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

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              10Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20

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              “Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20” Metadata:

              • Title: ➤  Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
              • Author:
              • Language: English
              • Number of Pages: Median: 151
              • Publisher: ➤  National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
              • Publish Date:
              • Publish Location: ➤  [Washington, DC] - [Springfield, Va - Hampton, Va

              “Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1986
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

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                11Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds

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                “Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds” Metadata:

                • Title: ➤  Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds
                • Author:
                • Language: English
                • Publisher: ➤  For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division
                • Publish Date:
                • Publish Location: ➤  [Washington, DC] - Hampton, Va - [Springfield, Va

                “Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1987
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

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                  12Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows

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                  “Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Metadata:

                  • Title: ➤  Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 180
                  • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
                  • Publish Date:
                  • Publish Location: ➤  [Springfield, Va - Hampton, Va - [Washington, D.C.]

                  “Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1986
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Access

                  Downloads Are Not Available:

                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                    13Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson

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                    “Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson” Metadata:

                    • Title: ➤  Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 69
                    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service, 1978.
                    • Publish Date:
                    • Publish Location: Washington - Springfield, Va

                    “Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1978
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

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                    14Venturi nozzle effects on fuel drop size and nitrogen oxide emissions

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                    “Venturi nozzle effects on fuel drop size and nitrogen oxide emissions” Metadata:

                    • Title: ➤  Venturi nozzle effects on fuel drop size and nitrogen oxide emissions
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 14
                    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                    • Publish Date:
                    • Publish Location: ➤  Washington, D.C - [Springfield, Va

                    “Venturi nozzle effects on fuel drop size and nitrogen oxide emissions” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1982
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

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                    15TMI-2 nozzle examinations performed at the Idaho National Laboratory

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                    “TMI-2 nozzle examinations performed at the Idaho National Laboratory” Metadata:

                    • Title: ➤  TMI-2 nozzle examinations performed at the Idaho National Laboratory
                    • Author:
                    • Language: English
                    • Publisher: ➤  Division of Systems Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission - Supt. of Docs., U.S. G.P.O. [distributor]
                    • Publish Date:
                    • Publish Location: Washington, DC

                    “TMI-2 nozzle examinations performed at the Idaho National Laboratory” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1994
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

                    Online Access

                    Downloads Are Not Available:

                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                      16Two-dimensional nozzle plume characteristics

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                      “Two-dimensional nozzle plume characteristics” Metadata:

                      • Title: ➤  Two-dimensional nozzle plume characteristics
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
                      • Publish Date:
                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                      “Two-dimensional nozzle plume characteristics” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1987
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

                      Online Access

                      Downloads Are Not Available:

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                        17Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles

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                        “Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles” Metadata:

                        • Title: ➤  Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 181
                        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office
                        • Publish Date:
                        • Publish Location: ➤  Springfield, Va. : for sale by the National Technical Information Service - [Washington]

                        “Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1978
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

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                        18Wake adapted ducted propellers

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                        “Wake adapted ducted propellers” Metadata:

                        • Title: Wake adapted ducted propellers
                        • Author: ➤  
                        • Language: English
                        • Number of Pages: Median: 130
                        • Publisher: ➤  Veenman & Zonen - Netherlands Ship Model Basin
                        • Publish Date:
                        • Publish Location: Wageningen

                        “Wake adapted ducted propellers” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1970
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

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                        19Analysis of film cooling in rocket nozzles

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                        “Analysis of film cooling in rocket nozzles” Metadata:

                        • Title: ➤  Analysis of film cooling in rocket nozzles
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Technical Information Service, distributor - University of Alabama, College of Engineering, Bureau of Engineering Research - National Aeronautics and Space Administration
                        • Publish Date:
                        • Publish Location: ➤  [Washington, DC - Springfield, Va - Tuscaloosa, Ala

                        “Analysis of film cooling in rocket nozzles” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1993
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Access

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                          20A bibliographical survey of flow through orifices and parallel-throated nozzles

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                          “A bibliographical survey of flow through orifices and parallel-throated nozzles” Metadata:

                          • Title: ➤  A bibliographical survey of flow through orifices and parallel-throated nozzles
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 197
                          • Publisher: Chapman & Hall
                          • Publish Date:
                          • Publish Location: London

                          “A bibliographical survey of flow through orifices and parallel-throated nozzles” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1952
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          21Development of a code for wall contour design in the transonic region of axisymmetric and square nozzles

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                          “Development of a code for wall contour design in the transonic region of axisymmetric and square nozzles” Metadata:

                          • Title: ➤  Development of a code for wall contour design in the transonic region of axisymmetric and square nozzles
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                          • Publish Date:
                          • Publish Location: ➤  Springfield, Va - [Washington, DC

                          “Development of a code for wall contour design in the transonic region of axisymmetric and square nozzles” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1994
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

                          Online Access

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                            22Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft

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                            “Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft” Metadata:

                            • Title: ➤  Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                            “Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1993
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

                            Online Access

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                              23Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft

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                              “Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft” Metadata:

                              • Title: ➤  Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft
                              • Author:
                              • Language: English
                              • Number of Pages: Median: 14
                              • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                              • Publish Date:
                              • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                              “Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1992
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

                              Online Access

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                                24Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps

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                                “Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps” Metadata:

                                • Title: ➤  Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps
                                • Author:
                                • Language: English
                                • Number of Pages: Median: 33
                                • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration,Scientific and Technical Information Branch
                                • Publish Date:
                                • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                “Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1982
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                25Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration

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                                “Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration” Metadata:

                                • Title: ➤  Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration
                                • Author:
                                • Language: English
                                • Number of Pages: Median: 104
                                • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                                • Publish Date:
                                • Publish Location: ➤  Washington, D.C - [Springfield, Va

                                “Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1984
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                26Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows

                                By

                                “Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Metadata:

                                • Title: ➤  Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows
                                • Author:
                                • Language: English
                                • Number of Pages: Median: 180
                                • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
                                • Publish Date:
                                • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                “Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1986
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                  27First NASA/Industry High Speed Research Program Nozzle Symposium

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                                  “First NASA/Industry High Speed Research Program Nozzle Symposium” Metadata:

                                  • Title: ➤  First NASA/Industry High Speed Research Program Nozzle Symposium
                                  • Author: ➤  
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service [distributor
                                  • Publish Date:
                                  • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA

                                  “First NASA/Industry High Speed Research Program Nozzle Symposium” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1999
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                    28An aid to the design of orifice plates according to ISO code 5167

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                                    “An aid to the design of orifice plates according to ISO code 5167” Metadata:

                                    • Title: ➤  An aid to the design of orifice plates according to ISO code 5167
                                    • Author:
                                    • Language: English
                                    • Number of Pages: Median: 33
                                    • Publisher: ➤  University of New South Wales, Water Research Laboratory
                                    • Publish Date:
                                    • Publish Location: Manly Vale, N.S.W., Australia

                                    “An aid to the design of orifice plates according to ISO code 5167” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1988
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

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                                    29Low thrust viscous nozzle flow fields prediction

                                    By

                                    “Low thrust viscous nozzle flow fields prediction” Metadata:

                                    • Title: ➤  Low thrust viscous nozzle flow fields prediction
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                    • Publish Date:
                                    • Publish Location: ➤  [Springfield, Va - [Washington, DC

                                    “Low thrust viscous nozzle flow fields prediction” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1988
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

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                                      30Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊

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                                      “Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊” Metadata:

                                      • Title: ➤  Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
                                      • Publish Date:
                                      • Publish Location: Hampton, Va - Springfield, VA

                                      “Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

                                      • First Year Published: 1995
                                      • Is Full Text Available: No
                                      • Is The Book Public: No
                                      • Access Status: No_ebook

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                                        31Additional support for the TDK/MABL computer program

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                                        “Additional support for the TDK/MABL computer program” Metadata:

                                        • Title: ➤  Additional support for the TDK/MABL computer program
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  George C. Marshall Space Flight Center, National Aeronautics and Space Administration
                                        • Publish Date:
                                        • Publish Location: ➤  Marshall Space Flight Center, AL

                                        “Additional support for the TDK/MABL computer program” Subjects and Themes:

                                        Edition Identifiers:

                                        Access and General Info:

                                        • First Year Published: 1993
                                        • Is Full Text Available: No
                                        • Is The Book Public: No
                                        • Access Status: No_ebook

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                                          32Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20

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                                          “Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20” Metadata:

                                          • Title: ➤  Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                          • Publish Date:
                                          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                          “Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1992
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

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                                            33Analysis of internal flow in a ventral nozzle for STOVL aircraft

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                                            “Analysis of internal flow in a ventral nozzle for STOVL aircraft” Metadata:

                                            • Title: ➤  Analysis of internal flow in a ventral nozzle for STOVL aircraft
                                            • Author:
                                            • Language: English
                                            • Number of Pages: Median: 19
                                            • Publisher: ➤  For sale by the National Technical Information Service - NASA
                                            • Publish Date:
                                            • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                            “Analysis of internal flow in a ventral nozzle for STOVL aircraft” Subjects and Themes:

                                            Edition Identifiers:

                                            Access and General Info:

                                            • First Year Published: 1990
                                            • Is Full Text Available: No
                                            • Is The Book Public: No
                                            • Access Status: No_ebook

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                                              34Modifications to the nozzle test chamber to extend nozzle static-test capability

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                                              “Modifications to the nozzle test chamber to extend nozzle static-test capability” Metadata:

                                              • Title: ➤  Modifications to the nozzle test chamber to extend nozzle static-test capability
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                              • Publish Date:
                                              • Publish Location: [Washington, D.C.?]

                                              “Modifications to the nozzle test chamber to extend nozzle static-test capability” Subjects and Themes:

                                              Edition Identifiers:

                                              Access and General Info:

                                              • First Year Published: 1985
                                              • Is Full Text Available: No
                                              • Is The Book Public: No
                                              • Access Status: No_ebook

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                                                35Nuclear thermal rocket nozzle testing and evaluation program

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                                                “Nuclear thermal rocket nozzle testing and evaluation program” Metadata:

                                                • Title: ➤  Nuclear thermal rocket nozzle testing and evaluation program
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                                                • Publish Date:
                                                • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                “Nuclear thermal rocket nozzle testing and evaluation program” Subjects and Themes:

                                                Edition Identifiers:

                                                Access and General Info:

                                                • First Year Published: 1993
                                                • Is Full Text Available: No
                                                • Is The Book Public: No
                                                • Access Status: No_ebook

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                                                  36Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards

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                                                  “Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards” Metadata:

                                                  • Title: ➤  Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards
                                                  • Author:
                                                  • Language: English
                                                  • Number of Pages: Median: 73
                                                  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                                                  • Publish Date:
                                                  • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                                  “Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards” Subjects and Themes:

                                                  Edition Identifiers:

                                                  Access and General Info:

                                                  • First Year Published: 1983
                                                  • Is Full Text Available: No
                                                  • Is The Book Public: No
                                                  • Access Status: No_ebook

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                                                  37Design and Navier-Stokes analysis of hypersonic wind tunnel nozzles

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                                                  “Design and Navier-Stokes analysis of hypersonic wind tunnel nozzles” Metadata:

                                                  • Title: ➤  Design and Navier-Stokes analysis of hypersonic wind tunnel nozzles
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  National Aeronautics and Space Administration]
                                                  • Publish Date:
                                                  • Publish Location: [Washington, DC

                                                  “Design and Navier-Stokes analysis of hypersonic wind tunnel nozzles” Subjects and Themes:

                                                  Edition Identifiers:

                                                  Access and General Info:

                                                  • First Year Published: 1989
                                                  • Is Full Text Available: No
                                                  • Is The Book Public: No
                                                  • Access Status: No_ebook

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                                                    38Liquid rocket engine nozzles

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                                                    “Liquid rocket engine nozzles” Metadata:

                                                    • Title: Liquid rocket engine nozzles
                                                    • Author:
                                                    • Number of Pages: Median: 112
                                                    • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                                                    • Publish Location: Springfield, Va - Washington

                                                    “Liquid rocket engine nozzles” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

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                                                    39Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson

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                                                    “Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson” Metadata:

                                                    • Title: ➤  Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson
                                                    • Author:
                                                    • Language: English
                                                    • Number of Pages: Median: 69
                                                    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
                                                    • Publish Date:
                                                    • Publish Location: Washington - Springfield, Va

                                                    “Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1978
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

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                                                    40Shape optimization governed by the Euler equations using an adjoint method

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                                                    “Shape optimization governed by the Euler equations using an adjoint method” Metadata:

                                                    • Title: ➤  Shape optimization governed by the Euler equations using an adjoint method
                                                    • Author:
                                                    • Language: English
                                                    • Number of Pages: Median: 18
                                                    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Institute for Computer Applications in Science and Engineering - National Technical Information Service, distributor
                                                    • Publish Date:
                                                    • Publish Location: [Springfield, Va - Hampton, Va

                                                    “Shape optimization governed by the Euler equations using an adjoint method” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1993
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

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                                                    41Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off design conditions

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                                                    “Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off design conditions” Metadata:

                                                    • Title: ➤  Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off design conditions
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                                                    • Publish Date:
                                                    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                                    “Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off design conditions” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1988
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

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                                                      42Viscous three-dimensional analyses for nozzles for hypersonic propulsion

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                                                      “Viscous three-dimensional analyses for nozzles for hypersonic propulsion” Metadata:

                                                      • Title: ➤  Viscous three-dimensional analyses for nozzles for hypersonic propulsion
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  Sverdrup Technology, Inc., NASA Lewis Research Center Group - For sale by the National Technical Information Service
                                                      • Publish Date:
                                                      • Publish Location: ➤  [Springfield, Va - Cleveland, Ohio

                                                      “Viscous three-dimensional analyses for nozzles for hypersonic propulsion” Subjects and Themes:

                                                      Edition Identifiers:

                                                      Access and General Info:

                                                      • First Year Published: 1990
                                                      • Is Full Text Available: No
                                                      • Is The Book Public: No
                                                      • Access Status: No_ebook

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                                                        43Transonic flow in the throat region of an annular nozzle with an arbitrary smooth profile

                                                        By

                                                        “Transonic flow in the throat region of an annular nozzle with an arbitrary smooth profile” Metadata:

                                                        • Title: ➤  Transonic flow in the throat region of an annular nozzle with an arbitrary smooth profile
                                                        • Author:
                                                        • Language: English
                                                        • Number of Pages: Median: 30
                                                        • Publisher: H.M.S.O.
                                                        • Publish Date:
                                                        • Publish Location: London

                                                        “Transonic flow in the throat region of an annular nozzle with an arbitrary smooth profile” Subjects and Themes:

                                                        Edition Identifiers:

                                                        • The Open Library ID: OL5589224M
                                                        • Online Computer Library Center (OCLC) ID: 11143317
                                                        • Library of Congress Control Number (LCCN): 67110477

                                                        Access and General Info:

                                                        • First Year Published: 1967
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
                                                        • Access Status: No_ebook

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                                                        44Computer program for the numerical solution of nonequilibrium expansions of reacting gas mixtures

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                                                        “Computer program for the numerical solution of nonequilibrium expansions of reacting gas mixtures” Metadata:

                                                        • Title: ➤  Computer program for the numerical solution of nonequilibrium expansions of reacting gas mixtures
                                                        • Author:
                                                        • Language: English
                                                        • Number of Pages: Median: 142
                                                        • Publisher: ➤  For sale by the Clearinghouse for Federal Scientific and Technical Information
                                                        • Publish Date:
                                                        • Publish Location: Springfield, Va

                                                        “Computer program for the numerical solution of nonequilibrium expansions of reacting gas mixtures” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

                                                        • First Year Published: 1966
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
                                                        • Access Status: No_ebook

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                                                        45Induction plasma nozzle tests

                                                        By

                                                        “Induction plasma nozzle tests” Metadata:

                                                        • Title: Induction plasma nozzle tests
                                                        • Author:
                                                        • Language: English
                                                        • Number of Pages: Median: 45
                                                        • Publisher: ➤  National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.]
                                                        • Publish Date:
                                                        • Publish Location: Washington

                                                        “Induction plasma nozzle tests” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

                                                        • First Year Published: 1971
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
                                                        • Access Status: No_ebook

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                                                        46An investigation of the Doble needle regulating nozzle

                                                        By

                                                        “An investigation of the Doble needle regulating nozzle” Metadata:

                                                        • Title: ➤  An investigation of the Doble needle regulating nozzle
                                                        • Author:
                                                        • Language: English
                                                        • Number of Pages: Median: 30
                                                        • Publisher: A. Doble co.
                                                        • Publish Date:
                                                        • Publish Location: San Francisco

                                                        “An investigation of the Doble needle regulating nozzle” Subjects and Themes:

                                                        Edition Identifiers:

                                                        • The Open Library ID: OL6991308M
                                                        • Online Computer Library Center (OCLC) ID: 20860874
                                                        • Library of Congress Control Number (LCCN): 07039118

                                                        Access and General Info:

                                                        • First Year Published: 1904
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
                                                        • Access Status: No_ebook

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                                                        47FNAS/Summer faculty Fellowshop Research Continuation Program task #3 entitled analysis of film cooling in rocket nozzle

                                                        By

                                                        “FNAS/Summer faculty Fellowshop Research Continuation Program task #3 entitled analysis of film cooling in rocket nozzle” Metadata:

                                                        • Title: ➤  FNAS/Summer faculty Fellowshop Research Continuation Program task #3 entitled analysis of film cooling in rocket nozzle
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                        • Publish Date:
                                                        • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                        “FNAS/Summer faculty Fellowshop Research Continuation Program task #3 entitled analysis of film cooling in rocket nozzle” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

                                                        • First Year Published: 1992
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
                                                        • Access Status: No_ebook

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                                                          48Analysis of supersonic plug nozzle flowfield and heat transfer

                                                          By

                                                          “Analysis of supersonic plug nozzle flowfield and heat transfer” Metadata:

                                                          • Title: ➤  Analysis of supersonic plug nozzle flowfield and heat transfer
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
                                                          • Publish Date:
                                                          • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                                          “Analysis of supersonic plug nozzle flowfield and heat transfer” Subjects and Themes:

                                                          Edition Identifiers:

                                                          Access and General Info:

                                                          • First Year Published: 1989
                                                          • Is Full Text Available: No
                                                          • Is The Book Public: No
                                                          • Access Status: No_ebook

                                                          Online Access

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                                                            49Review of industry efforts to manage pressurized water reactor feedwater nozzle, piping, and feedring cracking and wall thinning

                                                            By

                                                            “Review of industry efforts to manage pressurized water reactor feedwater nozzle, piping, and feedring cracking and wall thinning” Metadata:

                                                            • Title: ➤  Review of industry efforts to manage pressurized water reactor feedwater nozzle, piping, and feedring cracking and wall thinning
                                                            • Author:
                                                            • Language: English
                                                            • Number of Pages: Median: 159
                                                            • Publisher: ➤  U.S. Nuclear Regulatory Commission
                                                            • Publish Date:
                                                            • Publish Location: Washington, DC

                                                            “Review of industry efforts to manage pressurized water reactor feedwater nozzle, piping, and feedring cracking and wall thinning” Subjects and Themes:

                                                            Edition Identifiers:

                                                            Access and General Info:

                                                            • First Year Published: 1997
                                                            • Is Full Text Available: No
                                                            • Is The Book Public: No
                                                            • Access Status: No_ebook

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                                                            50Hydraulic experiments with valves, orifices, hose, nozzles, and orifice buckets

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                                                            Book's cover

                                                            “Hydraulic experiments with valves, orifices, hose, nozzles, and orifice buckets” Metadata:

                                                            • Title: ➤  Hydraulic experiments with valves, orifices, hose, nozzles, and orifice buckets
                                                            • Author: ➤  
                                                            • Language: English
                                                            • Number of Pages: Median: 80
                                                            • Publisher: ➤  University of Illlinois - University of Illinois
                                                            • Publish Date:
                                                            • Publish Location: Urbana, Ill

                                                            “Hydraulic experiments with valves, orifices, hose, nozzles, and orifice buckets” Subjects and Themes:

                                                            Edition Identifiers:

                                                            Access and General Info:

                                                            • First Year Published: 1918
                                                            • Is Full Text Available: Yes
                                                            • Is The Book Public: Yes
                                                            • Access Status: Public

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