Explore: Intake Systems

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Source: The Open Library

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1Computation of multi-dimensional viscous supersonic jet flow

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“Computation of multi-dimensional viscous supersonic jet flow” Metadata:

  • Title: ➤  Computation of multi-dimensional viscous supersonic jet flow
  • Author:
  • Language: English
  • Number of Pages: Median: 124
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Lewis Research Center - For sale by the National Technical Information Service
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Washington, D.C.] - Cleveland, Ohio

“Computation of multi-dimensional viscous supersonic jet flow” 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

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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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    2The structural dynamics analysis of the main injector LOX inlet tee and its redesign

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    “The structural dynamics analysis of the main injector LOX inlet tee and its redesign” Metadata:

    • Title: ➤  The structural dynamics analysis of the main injector LOX inlet tee and its redesign
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration?. - National Aeronautics and Space Administration? - Rockwell International, Rocketdyne Division?
    • Publish Date:
    • Publish Location: ➤  [Canoga Park, Calif - Washington, D.C

    “The structural dynamics analysis of the main injector LOX inlet tee and its redesign” 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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      3Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane

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      “Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane” Metadata:

      • Title: ➤  Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  Edwards, Calif - [Springfield, Va

      “Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane” 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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        4Hydrodynamic design of the fastrac turbopump

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        “Hydrodynamic design of the fastrac turbopump” Metadata:

        • Title: ➤  Hydrodynamic design of the fastrac turbopump
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Washington, D.C

        “Hydrodynamic design of the fastrac turbopump” 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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          5Numerical and analytical study of the inlet startup process in a shock tunnel environment

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          “Numerical and analytical study of the inlet startup process in a shock tunnel environment” Metadata:

          • Title: ➤  Numerical and analytical study of the inlet startup process in a shock tunnel environment
          • Author:
          • Publisher: AIAA
          • Publish Date:
          • Publish Location: New York

          “Numerical and analytical study of the inlet startup process in a shock tunnel environment” 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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          6Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack

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          “Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack” Metadata:

          • Title: ➤  Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

          “Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack” 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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            7Unsteady ejector performance

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            “Unsteady ejector performance” Metadata:

            • Title: Unsteady ejector performance
            • Author:
            • Language: English
            • Publisher: ➤  Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Glenn Research Center
            • Publish Date:
            • Publish Location: Cleveland, Ohio - Hanover MD

            “Unsteady ejector performance” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 2002
            • 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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              8Intake and exhaust noise

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              “Intake and exhaust noise” Metadata:

              • Title: Intake and exhaust noise
              • Author:
              • Number of Pages: Median: 18
              • Publisher: ➤  University of Southampton, Institute of Sound and Vibration Research
              • Publish Date:
              • Publish Location: Southampton, England

              “Intake and exhaust noise” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

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              9Piston engine intake and exhaust system design

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              “Piston engine intake and exhaust system design” Metadata:

              • Title: ➤  Piston engine intake and exhaust system design
              • Author:
              • Number of Pages: Median: 49
              • Publisher: ➤  University of Southampton, Institute of Sound and Vibration Research
              • Publish Date:
              • Publish Location: Southampton

              “Piston engine intake and exhaust system design” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

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              10Intakes and boundary layer crossflows for hypersonic vehicles

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              “Intakes and boundary layer crossflows for hypersonic vehicles” Metadata:

              • Title: ➤  Intakes and boundary layer crossflows for hypersonic vehicles
              • Author:
              • Number of Pages: Median: 11
              • Publisher: ➤  American Institute of Aeronautics and Astronautics
              • Publish Date:
              • Publish Location: New York

              “Intakes and boundary layer crossflows for hypersonic vehicles” 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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