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1Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel

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“Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” Metadata:

  • Title: ➤  Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: Hampton, Va - [Springfield, Va

“Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” 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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    2Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle

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    “Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle” Metadata:

    • Title: ➤  Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - MCAT Institute - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  San Jose, CA - Springfield, Va.? - [Washington, DC - [Washington, D.C - Springfield, Va

    “Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle” 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

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      3Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research

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      “Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research” Metadata:

      • Title: ➤  Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Washington, DC - Springfield, Va

      “Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research” 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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        4Supersonic laminar flow control research

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        “Supersonic laminar flow control research” Metadata:

        • Title: ➤  Supersonic laminar flow control research
        • Author:
        • Language: English
        • Publisher: ➤  Ames Research Center - National Aeronautics and Space Administration - University of Tennessee, Space Institute - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Tullahoma, TN - [Springfield, Va - Moffett Field, CA - [Washington, DC - Springfield, Va

        “Supersonic laminar flow control research” 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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          5Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure

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          “Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure” Metadata:

          • Title: ➤  Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: Hampton, Va - [Springfield, Va

          “Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1996
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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            6Aerodynamic design optimization via reduced Hessian SQP with solution refining

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            “Aerodynamic design optimization via reduced Hessian SQP with solution refining” Metadata:

            • Title: ➤  Aerodynamic design optimization via reduced Hessian SQP with solution refining
            • Author:
            • Language: English
            • Publisher: ➤  Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  [Washington, DC] - [Springfield, Va

            “Aerodynamic design optimization via reduced Hessian SQP with solution refining” 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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              7Nozzle thrust optimization while reducing jet noise

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              “Nozzle thrust optimization while reducing jet noise” Metadata:

              • Title: ➤  Nozzle thrust optimization while reducing jet noise
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
              • Publish Date:
              • Publish Location: ➤  [Washington, D.C - Springfield, Va

              “Nozzle thrust optimization while reducing jet noise” 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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                8First 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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                  9Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle

                  By

                  “Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle” Metadata:

                  • Title: ➤  Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Pratt and Whitney Aircraft
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - [West Palm Beach, Fla - Washington, DC

                  “Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle” 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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                    10Development of three-dimensional code for the analysis of jet mixing problem

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                    “Development of three-dimensional code for the analysis of jet mixing problem” Metadata:

                    • Title: ➤  Development of three-dimensional code for the analysis of jet mixing problem
                    • Author:
                    • Language: English
                    • Publisher: ➤  For sale by the National Technical Information Service
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - Washington, D.C

                    “Development of three-dimensional code for the analysis of jet mixing problem” 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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                      11The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows

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                      “The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows” Metadata:

                      • Title: ➤  The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                      • Publish Date:
                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                      “The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows” 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

                      Online Access

                      Downloads Are Not Available:

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                        12Dual-throat thruster thermal model

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                        “Dual-throat thruster thermal model” Metadata:

                        • Title: ➤  Dual-throat thruster thermal model
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Aeronautics and Space Administration, Marshall Space Flight Center, Alabama - Aerojet TechSystems Co. - National Technical Information Service, distributor
                        • Publish Date:
                        • Publish Location: ➤  [Springfield, Va - [Huntsville, Ala.] - Sacramento, Calif

                        “Dual-throat thruster thermal model” 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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                          13Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle

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                          “Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle” Metadata:

                          • Title: ➤  Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle
                          • 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

                          “Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle” 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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                            14Flight motor set 360L001 (STS-26R)

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                            “Flight motor set 360L001 (STS-26R)” Metadata:

                            • Title: ➤  Flight motor set 360L001 (STS-26R)
                            • Author:
                            • Language: English
                            • Publisher: ➤  Thiokol Corp., Space Operations - National Aeronautics and Space Administration, George C. Marshall Space Flight Center
                            • Publish Date:
                            • Publish Location: ➤  Marshall Space Flight Center, Ala - Brigham City, UT

                            “Flight motor set 360L001 (STS-26R)” 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

                            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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                              15Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air

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                              “Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air” Metadata:

                              • Title: ➤  Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air
                              • Author:
                              • Language: English
                              • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
                              • Publish Date:
                              • Publish Location: Hamtpon, Va - [Springfield, Va

                              “Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air” 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

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                                16High speed nozzles task

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                                “High speed nozzles task” Metadata:

                                • Title: High speed nozzles task
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Technical Information Service, distributor - University of Cincinnati - National Aeronautics and Space Administration
                                • Publish Date:
                                • Publish Location: ➤  Springfield, Va - [Cincinnati, Ohio?] - [Washington, DC

                                “High speed nozzles task” 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

                                Online Access

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                                  17Enhancement of mixing in a rectangular jet by mechanical tabs

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                                  “Enhancement of mixing in a rectangular jet by mechanical tabs” Metadata:

                                  • Title: ➤  Enhancement of mixing in a rectangular jet by mechanical tabs
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration
                                  • Publish Date:
                                  • Publish Location: [Washington, DC]

                                  “Enhancement of mixing in a rectangular jet by mechanical tabs” 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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                                    18Shear flow control of cold and heated rectangular jets by mechanical tabs

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                                    “Shear flow control of cold and heated rectangular jets by mechanical tabs” Metadata:

                                    • Title: ➤  Shear flow control of cold and heated rectangular jets by mechanical tabs
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                    • Publish Date:
                                    • Publish Location: ➤  [Washington, DC - Springfield, Va

                                    “Shear flow control of cold and heated rectangular jets by mechanical tabs” 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

                                    Downloads Are Not Available:

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                                      19A performance comparison of two small rocket nozzles

                                      By

                                      “A performance comparison of two small rocket nozzles” Metadata:

                                      • Title: ➤  A performance comparison of two small rocket nozzles
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                      • Publish Date:
                                      • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                      “A performance comparison of two small rocket nozzles” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

                                      • First Year Published: 1996
                                      • Is Full Text Available: No
                                      • Is The Book Public: No
                                      • Access Status: No_ebook

                                      Online Access

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                                        20Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities

                                        By

                                        “Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities” Metadata:

                                        • Title: ➤  Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities
                                        • Author:
                                        • Number of Pages: Median: 106
                                        • Publisher: NASA
                                        • Publish Date:
                                        • Publish Location: Washington

                                        “Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities” 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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                                        21Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf

                                        By

                                        “Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf” Metadata:

                                        • Title: ➤  Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf
                                        • 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

                                        “Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf” Subjects and Themes:

                                        Edition Identifiers:

                                        Access and General Info:

                                        • First Year Published: 1996
                                        • Is Full Text Available: No
                                        • Is The Book Public: No
                                        • Access Status: No_ebook

                                        Online Access

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                                          22Contoured nozzle design and evaluation for hotshot wind tunnels

                                          By

                                          “Contoured nozzle design and evaluation for hotshot wind tunnels” Metadata:

                                          • Title: ➤  Contoured nozzle design and evaluation for hotshot wind tunnels
                                          • Author:
                                          • Number of Pages: Median: 13
                                          • Publisher: AIAA
                                          • Publish Date:
                                          • Publish Location: New York

                                          “Contoured nozzle design and evaluation for hotshot wind tunnels” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1968
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

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                                          23Comparison of 3D computation and experiment for non-axisymmetric nozzles

                                          By

                                          “Comparison of 3D computation and experiment for non-axisymmetric nozzles” Metadata:

                                          • Title: ➤  Comparison of 3D computation and experiment for non-axisymmetric nozzles
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                          • Publish Date:
                                          • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                          “Comparison of 3D computation and experiment for non-axisymmetric 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

                                          Online Access

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                                          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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                                            24Nozzle design optimization by method-of-characteristics

                                            By

                                            “Nozzle design optimization by method-of-characteristics” Metadata:

                                            • Title: ➤  Nozzle design optimization by method-of-characteristics
                                            • Author:
                                            • Number of Pages: Median: 11
                                            • Publisher: ➤  American Institute of Aeronautics and Astronautics
                                            • Publish Date:
                                            • Publish Location: Washington, D. C

                                            “Nozzle design optimization by method-of-characteristics” 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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                                            25Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)

                                            By

                                            “Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)” Metadata:

                                            • Title: ➤  Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
                                            • Author:
                                            • Number of Pages: Median: 21
                                            • Publisher: Lewis Research Center
                                            • Publish Date:
                                            • Publish Location: Cleveland, Ohio

                                            “Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)” 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

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                                            26Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability

                                            By

                                            “Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability” Metadata:

                                            • Title: ➤  Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
                                            • Publish Date:
                                            • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                            “Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability” 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

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                                              27Advanced small rocket chambers option 3

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                                              “Advanced small rocket chambers option 3” Metadata:

                                              • Title: ➤  Advanced small rocket chambers option 3
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                              • Publish Date:
                                              • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                              “Advanced small rocket chambers option 3” 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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                                                28Analysis and design of optimized truncated scarfed nozzles subject to external flow effects

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                                                “Analysis and design of optimized truncated scarfed nozzles subject to external flow effects” Metadata:

                                                • Title: ➤  Analysis and design of optimized truncated scarfed nozzles subject to external flow effects
                                                • Author:
                                                • Language: English
                                                • Number of Pages: Median: 10
                                                • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
                                                • Publish Date:
                                                • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                                “Analysis and design of optimized truncated scarfed nozzles subject to external flow effects” 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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                                                  29Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows

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                                                  “Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows” Metadata:

                                                  • Title: ➤  Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                  • Publish Date:
                                                  • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                  “Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows” Subjects and Themes:

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                                                  Access and General Info:

                                                  • First Year Published: 1998
                                                  • Is Full Text Available: No
                                                  • Is The Book Public: No
                                                  • Access Status: No_ebook

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                                                    30Decomposing solid micropropulsion nozzle performance issues

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                                                    “Decomposing solid micropropulsion nozzle performance issues” Metadata:

                                                    • Title: ➤  Decomposing solid micropropulsion nozzle performance issues
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  Available from the NASA Center for Aerospace Information - National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center
                                                    • Publish Date:
                                                    • Publish Location: ➤  Springfield, VA - [Cleveland, Ohio] - Hanover, MD

                                                    “Decomposing solid micropropulsion nozzle performance issues” Subjects and Themes:

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                                                    • First Year Published: 2003
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

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                                                      31Collective interaction in a linear array of supersonic rectangular jets

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                                                      “Collective interaction in a linear array of supersonic rectangular jets” Metadata:

                                                      • Title: ➤  Collective interaction in a linear array of supersonic rectangular jets
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
                                                      • Publish Date:
                                                      • Publish Location: ➤  Springfield, VA - [Cleveland, Ohio]

                                                      “Collective interaction in a linear array of supersonic rectangular jets” Subjects and Themes:

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                                                      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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                                                        32NPAC--nozzle performance analysis code

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                                                        “NPAC--nozzle performance analysis code” Metadata:

                                                        • Title: ➤  NPAC--nozzle performance analysis code
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                        • Publish Date:
                                                        • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                        “NPAC--nozzle performance analysis code” Subjects and Themes:

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                                                        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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                                                          33Velocity and temperature decay characteristics of inverted-profile jets

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                                                          “Velocity and temperature decay characteristics of inverted-profile jets” Metadata:

                                                          • Title: ➤  Velocity and temperature decay characteristics of inverted-profile jets
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
                                                          • Publish Date:
                                                          • Publish Location: [Cleveland, Ohio

                                                          “Velocity and temperature decay characteristics of inverted-profile jets” 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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                                                            34Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle

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                                                            “Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle” Metadata:

                                                            • Title: ➤  Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle
                                                            • Author:
                                                            • Number of Pages: Median: 24
                                                            • Publisher: Lewis Research Center
                                                            • Publish Date:
                                                            • Publish Location: Cleveland, Ohio

                                                            “Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle” 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

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                                                            35Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle

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                                                            “Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle” Metadata:

                                                            • Title: ➤  Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle
                                                            • Author:
                                                            • Language: English
                                                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                            • Publish Date:
                                                            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                                            “Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle” 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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                                                              36An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles

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                                                              “An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles” Metadata:

                                                              • Title: ➤  An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles
                                                              • 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

                                                              “An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles” 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

                                                              Online Access

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                                                                37Space shuttle production verification motor-1 (PV-1) static fire

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                                                                “Space shuttle production verification motor-1 (PV-1) static fire” Metadata:

                                                                • Title: ➤  Space shuttle production verification motor-1 (PV-1) static fire
                                                                • Author:
                                                                • Language: English
                                                                • Publisher: ➤  Thiokol Corp., Space Operations - National Aeronautics and Space Administration, George C. Marshall Space Flight Center
                                                                • Publish Date:
                                                                • Publish Location: ➤  Marshall Space Flight Center, Ala - Brigham City, UT

                                                                “Space shuttle production verification motor-1 (PV-1) static fire” 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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                                                                  38Space shuttle ice suppression system validation

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                                                                  “Space shuttle ice suppression system validation” Metadata:

                                                                  • Title: ➤  Space shuttle ice suppression system validation
                                                                  • Author:
                                                                  • Language: English
                                                                  • Publisher: ➤  Texas Engineering Experiment Station, Texas A&M University
                                                                  • Publish Date:
                                                                  • Publish Location: College Station, Tex

                                                                  “Space shuttle ice suppression system validation” 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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                                                                    39Design of an axisymmetric, contoured nozzle for the HEG

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                                                                    “Design of an axisymmetric, contoured nozzle for the HEG” Metadata:

                                                                    • Title: ➤  Design of an axisymmetric, contoured nozzle for the HEG
                                                                    • Author:
                                                                    • Number of Pages: Median: 71
                                                                    • Publisher: ➤  Deutsche Forschungsanstalt fur Luft- und Raumfahrt
                                                                    • Publish Date:
                                                                    • Publish Location: Koln, Germany

                                                                    “Design of an axisymmetric, contoured nozzle for the HEG” 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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