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Source: The Open Library

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1Numerical simulation of shock/turbulent boundary layer interaction

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“Numerical simulation of shock/turbulent boundary layer interaction” Metadata:

  • Title: ➤  Numerical simulation of shock/turbulent boundary layer interaction
  • Author:
  • Language: English
  • Publisher: ➤  Dept. of Aerospace Engineering Sciences, University of Colorado - National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C - Boulder, Colo - Springfield, Va

“Numerical simulation of shock/turbulent boundary layer interaction” 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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    2A pseudo-sound constitutive relationship for the dilatational covariances in compressible turbulence

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    “A pseudo-sound constitutive relationship for the dilatational covariances in compressible turbulence” Metadata:

    • Title: ➤  A pseudo-sound constitutive relationship for the dilatational covariances in compressible turbulence
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, VA - [Springfield, Va

    “A pseudo-sound constitutive relationship for the dilatational covariances in compressible turbulence” 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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      3Oscillating flow and heat transfer in a channel with sudden cross section change

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      “Oscillating flow and heat transfer in a channel with sudden cross section change” Metadata:

      • Title: ➤  Oscillating flow and heat transfer in a channel with sudden cross section change
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - [Washington, D.C

      “Oscillating flow and heat transfer in a channel with sudden cross section change” 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

      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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        4Energy transfer in compressible turbulence

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        “Energy transfer in compressible turbulence” Metadata:

        • Title: ➤  Energy transfer in compressible turbulence
        • Author:
        • Language: English
        • Publisher: ➤  Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: Hampton, VA - [Springfield, Va

        “Energy transfer in compressible turbulence” 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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          5The stability of compressible mixing layers in binary cases

          “The stability of compressible mixing layers in binary cases” Metadata:

          • Title: ➤  The stability of compressible mixing layers in binary cases
          • Language: English
          • Publisher: ➤  Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: Hampton, VA - [Springfield, Va

          “The stability of compressible mixing layers in binary cases” 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

          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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            Wiki

            Source: Wikipedia

            Wikipedia Results

            Search Results from Wikipedia

            Compressibility

            the compressibility (also known as the coefficient of compressibility or, if the temperature is held constant, the isothermal compressibility) is a

            Mach number

            Lockheed when reporting the effects of compressibility on the P-38 aircraft in 1942. Mach number is a measure of the compressibility characteristics of fluid

            Aerodynamics

            the effects of compressibility. Compressibility is a description of the amount of change of density in the flow. When the effects of compressibility on

            High-speed flight

            reality, air is compressible and viscous. While the effects of these properties are negligible at low speeds, compressibility effects in particular become

            Real gas

            taken into account: compressibility effects; variable specific heat capacity; van der Waals forces; non-equilibrium thermodynamic effects; issues with molecular

            Gas

            the assumption that the compressibility factor Z is set to 1 meaning that this pneumatic ratio remains constant. A compressibility factor of one also requires

            Ryan FR Fireball

            showed that the wing structure was not strong enough to resist compressibility effects. This was cured by doubling the number of rivets in the outer wing

            Fluid dynamics

            flow pressure becomes). Acoustic problems always require allowing compressibility, since sound waves are compression waves involving changes in pressure

            Wave drag

            sound barrier. Wave drag is a component of pressure drag due to compressibility effects. It is caused by the formation of shock waves around a body. Shock

            Compressibility factor

            before compressibility can be calculated. Alternatively, the compressibility factor for specific gases can be read from generalized compressibility charts