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Source: The Open Library

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1Performance 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

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    2Pitot-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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      3Ultra-high bypass ratio jet noise

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      “Ultra-high bypass ratio jet noise” Metadata:

      • Title: ➤  Ultra-high bypass ratio jet noise
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

      “Ultra-high bypass ratio jet noise” 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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        4Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft

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        “Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft” Metadata:

        • Title: ➤  Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

        “Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft” 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:

        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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          5Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

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          “Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control” Metadata:

          • Title: ➤  Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
          • 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 performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control” 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:

          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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            6Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft

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            “Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft” Metadata:

            • Title: ➤  Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft
            • Author:
            • Language: English
            • Number of Pages: Median: 14
            • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

            “Experimental and analytical study of close-coupled ventral nozzles for ASTOVL 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

            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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              7Experimental 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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                8Start up research effort in fluid mechanics

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                “Start up research effort in fluid mechanics” Metadata:

                • Title: ➤  Start up research effort in fluid mechanics
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                • Publish Date:
                • Publish Location: ➤  Springfield, Va - [Washington, DC

                “Start up research effort in fluid mechanics” 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

                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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                  9High 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

                  Downloads Are Not Available:

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                    10Shelf life extension for the lot AAE nozzle severance LSCs

                    By

                    “Shelf life extension for the lot AAE nozzle severance LSCs” Metadata:

                    • Title: ➤  Shelf life extension for the lot AAE nozzle severance LSCs
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Aeronautics and Space Administration, George C. Marshall Space Flight Center? - Thiokol Corp., Space Operations
                    • Publish Date:
                    • Publish Location: ➤  Brigham City, UT - [Marshall Space Flight Center, Ala

                    “Shelf life extension for the lot AAE nozzle severance LSCs” 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

                    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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                      11Separate flow nozzle test status meeting

                      “Separate flow nozzle test status meeting” Metadata:

                      • Title: ➤  Separate flow nozzle test status meeting
                      • Language: English
                      • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                      • Publish Date:
                      • Publish Location: [Washington, DC] - Hanover, MD

                      “Separate flow nozzle test status meeting” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 2000
                      • 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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                        12Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet

                        By

                        “Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Metadata:

                        • Title: ➤  Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
                        • 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

                        “Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” 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:

                        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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                          13Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case

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                          “Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case” Metadata:

                          • Title: ➤  Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                          “Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case” 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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                            14A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields

                            By

                            “A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields” Metadata:

                            • Title: ➤  A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
                            • Publish Date:
                            • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

                            “A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields” 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:

                            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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                              15An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct

                              By

                              “An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct” Metadata:

                              • Title: ➤  An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct
                              • Author:
                              • Language: English
                              • Publisher: Lewis Research Center
                              • Publish Date:
                              • Publish Location: [Cleveland, Ohio

                              “An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct” 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:

                              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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                                16Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector

                                By

                                “Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector” Metadata:

                                • Title: ➤  Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector
                                • 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

                                “Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector” 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

                                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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                                  17Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept

                                  By

                                  “Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept” Metadata:

                                  • Title: ➤  Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept
                                  • 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 performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept” 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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                                    18Analysis and design of optimized truncated scarfed nozzles subject to external flow effects

                                    By

                                    “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

                                    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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                                      19Titanium aluminide applications in the high speed civil transport

                                      By

                                      “Titanium aluminide applications in the high speed civil transport” Metadata:

                                      • Title: ➤  Titanium aluminide applications in the high speed civil transport
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
                                      • Publish Date:
                                      • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA

                                      “Titanium aluminide applications in the high speed civil transport” 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:

                                      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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                                        20Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility

                                        By

                                        “Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility” Metadata:

                                        • Title: ➤  Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - Available from the NASA Center for Aerospace Information
                                        • Publish Date:
                                        • Publish Location: ➤  [Cleveland, Ohio] - [Hanover, Md

                                        “Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility” Subjects and Themes:

                                        Edition Identifiers:

                                        Access and General Info:

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

                                        Online Access

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                                          21Separate flow nozzle test status meeting

                                          “Separate flow nozzle test status meeting” Metadata:

                                          • Title: ➤  Separate flow nozzle test status meeting
                                          • Language: English
                                          • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                          • Publish Date:
                                          • Publish Location: [Washington, DC] - Hanover, MD

                                          “Separate flow nozzle test status meeting” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 2000
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

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                                          22Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application

                                          By

                                          “Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application” Metadata:

                                          • Title: ➤  Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application
                                          • 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]

                                          “Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application” 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

                                          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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