Explore: Gas Injection

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Source: The Open Library

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1In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows

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“In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows” Metadata:

  • Title: ➤  In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor]
  • Publish Date:
  • Publish Location: ➤  Edwards, Calif - [Springfield, Va

“In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows” 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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    2Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation

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    “Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Metadata:

    • Title: ➤  Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
    • Author:
    • Language: English
    • Publisher: ➤  North Carolina State University, Dept. of Mechanical and Aerospace Engineering
    • Publish Date:
    • Publish Location: Raleigh, [N.C.]

    “Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” 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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      3Mixing of an airblast-atomized fuel spray injected into a crossflow of air

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      “Mixing of an airblast-atomized fuel spray injected into a crossflow of air” Metadata:

      • Title: ➤  Mixing of an airblast-atomized fuel spray injected into a crossflow of air
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
      • Publish Date:
      • Publish Location: ➤  Hanover, MD - [Cleveland, Ohio]

      “Mixing of an airblast-atomized fuel spray injected into a crossflow of air” 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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        4Investigation of mixing a supersonic stream with the flow downstream of a wedge

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        “Investigation of mixing a supersonic stream with the flow downstream of a wedge” Metadata:

        • Title: ➤  Investigation of mixing a supersonic stream with the flow downstream of a wedge
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Washington, DC

        “Investigation of mixing a supersonic stream with the flow downstream of a wedge” 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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          5Study of injection of helium into supersonic air flow using Rayleigh scattering

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          “Study of injection of helium into supersonic air flow using Rayleigh scattering” Metadata:

          • Title: ➤  Study of injection of helium into supersonic air flow using Rayleigh scattering
          • Author:
          • Language: English
          • Publish Date:

          “Study of injection of helium into supersonic air flow using Rayleigh scattering” 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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            6Combined tangential-normal injection into a supersonic flow

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            “Combined tangential-normal injection into a supersonic flow” Metadata:

            • Title: ➤  Combined tangential-normal injection into a supersonic flow
            • Author:
            • Number of Pages: Median: 12
            • Publisher: ➤  American Institute of Aeronautics and Astronautics
            • Publish Date:
            • Publish Location: Washington, D. C

            “Combined tangential-normal injection into a supersonic flow” 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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            7Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks

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            “Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks” Metadata:

            • Title: ➤  Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
            • Publish Date:
            • Publish Location: ➤  [Washington, DC] - [Springfield, Va

            “Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks” 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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