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Source: The Open Library

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1User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel

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“User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Metadata:

  • Title: ➤  User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
  • Author:
  • Language: English
  • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Washington, DC - [Springfield, Va - [Washington, DC] - Springfield, Va

“User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” 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

Online Access

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    2Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

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    “Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Metadata:

    • Title: ➤  Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
    • 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

    “Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” 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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      3Summary report of the orbital X-34 wing static aeroelastic study

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      “Summary report of the orbital X-34 wing static aeroelastic study” Metadata:

      • Title: ➤  Summary report of the orbital X-34 wing static aeroelastic study
      • Author:
      • Language: English
      • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va - Hanover, MD

      “Summary report of the orbital X-34 wing static aeroelastic study” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 2001
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

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        4Motion of the heliospheric termination shock at high heliographic latitude

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        “Motion of the heliospheric termination shock at high heliographic latitude” Metadata:

        • Title: ➤  Motion of the heliospheric termination shock at high heliographic latitude
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Washington, D.C - Springfield, Va

        “Motion of the heliospheric termination shock at high heliographic latitude” 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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          5A preliminary look at techniques used to obtain airdata from flight at high angles of attack

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          “A preliminary look at techniques used to obtain airdata from flight at high angles of attack” Metadata:

          • Title: ➤  A preliminary look at techniques used to obtain airdata from flight at high angles of attack
          • 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: ➤  [Springfield, Va - Edwards, Calif

          “A preliminary look at techniques used to obtain airdata from flight at high angles of attack” 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:

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            6Method for experimental determination of flutter speed by parameter identification

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            “Method for experimental determination of flutter speed by parameter identification” Metadata:

            • Title: ➤  Method for experimental determination of flutter speed by parameter identification
            • Author:
            • Language: English
            • Number of Pages: Median: 40
            • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C.] - Springfield, VA

            “Method for experimental determination of flutter speed by parameter identification” 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

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              7Pressure probe designs for dynamic pressure measurements in a supersonic flow field

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              “Pressure probe designs for dynamic pressure measurements in a supersonic flow field” Metadata:

              • Title: ➤  Pressure probe designs for dynamic pressure measurements in a supersonic flow field
              • 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

              “Pressure probe designs for dynamic pressure measurements in a supersonic flow field” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 2001
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

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                8Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel

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                “Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel” Metadata:

                • Title: ➤  Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
                • Author:
                • Language: English
                • Publisher: ➤  Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
                • Publish Date:
                • Publish Location: Hampton, Va - Hanover, MD

                “Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 2001
                • 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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                  9Demodulation system for fiber optic Bragg grating dynamic pressure sensing

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                  “Demodulation system for fiber optic Bragg grating dynamic pressure sensing” Metadata:

                  • Title: ➤  Demodulation system for fiber optic Bragg grating dynamic pressure sensing
                  • 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

                  “Demodulation system for fiber optic Bragg grating dynamic pressure sensing” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 2001
                  • 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

                    Dynamic pressure

                    In fluid dynamics, dynamic pressure (denoted by q or Q and sometimes called velocity pressure) is the quantity defined by: q = 1 2 ρ u 2 {\displaystyle

                    Max q

                    The max q, or maximum dynamic pressure, condition is the point when an aerospace vehicle's atmospheric flight reaches the maximum difference between the

                    Bernoulli's principle

                    pressure head) and p0 = p + q is the stagnation pressure (the sum of the static pressure p and dynamic pressure q). The constant in the Bernoulli equation

                    Stagnation pressure

                    equal to the dynamic pressure and static pressure combined. In compressible flows, stagnation pressure is also equal to total pressure as well, provided

                    Pressure measurement

                    dynamic pressures; this measurement is called the total pressure or stagnation pressure. Since dynamic pressure is referenced to static pressure, it is

                    Pressure

                    distributed. Gauge pressure (also spelled gage pressure) is the pressure relative to the ambient pressure. Various units are used to express pressure. Some of these

                    Pitot tube

                    static pressure as well it can be determined by the use of Bernoulli's equation which states: Stagnation pressure = static pressure + dynamic pressure Which

                    Static pressure

                    static pressure refers to a term in Bernoulli's equation written words as static pressure + dynamic pressure = total pressure. Since pressure measurements

                    Drag equation

                    P_{\rm {D}}A} where PD is the pressure exerted by the fluid on area A. Here the pressure PD is referred to as dynamic pressure due to the kinetic energy of

                    Water Resistant mark

                    properties of water and seawater, rapidly changing water pressure and temperature, as well as dynamic mechanical stresses encountered by a watch. Every "diver's"