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Source: The Open Library

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1Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

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“Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure” Metadata:

  • Title: ➤  Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

“Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure” 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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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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    2First 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

    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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      3Experimental 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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        4Experimental 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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          5Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20

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          “Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20” Metadata:

          • Title: ➤  Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
          • Author:
          • Language: English
          • Number of Pages: Median: 171
          • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Division
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

          “Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20” 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

          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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            6Decomposing 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:

            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

            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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              7Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance

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              “Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance” Metadata:

              • Title: ➤  Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
              • Publish Date:
              • Publish Location: ➤  [Springfield, Va - Edwards, Calif

              “Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1998
              • 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 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

                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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                  9An 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

                  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.

                  Online Borrowing:

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                    Find An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles at online marketplaces:


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