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Source: The Open Library

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1Hot-jet simulation in cryogenic wind tunnels

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“Hot-jet simulation in cryogenic wind tunnels” Metadata:

  • Title: ➤  Hot-jet simulation in cryogenic wind tunnels
  • Author:
  • Language: English
  • Number of Pages: Median: 45
  • Publisher: ➤  For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and SpaceAdministration - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
  • Publish Date:
  • Publish Location: ➤  Washington D.C - Hampton, Va - Washington, D.C - [Springfield, Va - [Washington, DC]

“Hot-jet simulation in cryogenic wind tunnels” 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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    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.

    Online Borrowing:

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      Find Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation at online marketplaces:


      3Radiation from advanced solid rocket motor plumes

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      “Radiation from advanced solid rocket motor plumes” Metadata:

      • Title: ➤  Radiation from advanced solid rocket motor plumes
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - SECA, Inc.
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - Huntsville, AL - [Washington, DC

      “Radiation from advanced solid rocket motor plumes” 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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        4Analysis of internal flow in a ventral nozzle for STOVL aircraft

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        “Analysis of internal flow in a ventral nozzle for STOVL aircraft” Metadata:

        • Title: ➤  Analysis of internal flow in a ventral nozzle for STOVL aircraft
        • Author:
        • Language: English
        • Number of Pages: Median: 19
        • Publisher: ➤  For sale by the National Technical Information Service - NASA
        • Publish Date:
        • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

        “Analysis of internal flow in a ventral nozzle for STOVL 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.

        Online Borrowing:

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          5High-altitude plume computer code development

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          “High-altitude plume computer code development” Metadata:

          • Title: ➤  High-altitude plume computer code development
          • Author:
          • Language: English
          • Publisher: ➤  Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center
          • Publish Date:
          • Publish Location: Huntsville, AL

          “High-altitude plume computer code development” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1985
          • 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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            6Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling

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            “Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling” Metadata:

            • Title: ➤  Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling
            • Author:
            • Number of Pages: Median: 34
            • Publisher: ➤  American Institute of Aeronautics and Astronautics
            • Publish Date:
            • Publish Location: Washington, D. C

            “Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling” 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

            Online Marketplaces

            Find Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling at online marketplaces:


            7Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes

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            “Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes” Metadata:

            • Title: ➤  Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes
            • Author:
            • Number of Pages: Median: 10
            • Publisher: ➤  American Institute of Aeronautics and Astronautics
            • Publish Date:
            • Publish Location: Washington, D. C

            “Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes” 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 Marketplaces

            Find Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes at online marketplaces:



            Wiki

            Source: Wikipedia

            Wikipedia Results

            Search Results from Wikipedia

            Airflow

            evacuates exhaust air. Air current Air flow meter Air handling unit Anemometer Atmosphere of Earth Computational fluid dynamics Damper (flow) Fluid dynamics

            Fluid dynamics

            equations. Direct numerical simulation (DNS), based on the Navier–Stokes equations, makes it possible to simulate turbulent flows at moderate Reynolds numbers

            Catalytic converter

            A catalytic converter part is an exhaust emission control device which converts toxic gases and pollutants in exhaust gas from an internal combustion engine

            List of computer simulation software

            of notable computer simulation software. Advanced Simulation Library - open-source hardware accelerated multiphysics simulation software. ASCEND - open-source

            Diesel particulate filter

            to remove diesel particulate matter or soot from the exhaust gas of a diesel engine. Wall-flow diesel particulate filters usually remove 85% or more

            Convection (heat transfer)

            of conduction (heat diffusion) and advection (heat transfer by bulk fluid flow). Convection is usually the dominant form of heat transfer in liquids and

            Heat recovery ventilation

            and cooling demands of buildings. By recovering the residual heat in the exhaust gas, the fresh air introduced into the air conditioning system is preheated

            Diving regulator

            by the ambient pressure of the exhaust and the flow resistance of the delivery system (mainly the umbilical and exhaust valve) and not much influenced

            Air flow bench

            for testing the intake and exhaust ports of cylinder heads of internal combustion engines. It is also used to test the flow capabilities of any component

            Back pressure

            to regulate flow of data, ensuring that components do not become overwhelmed. A common example of backpressure is that caused by the exhaust system (consisting