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1An arbitrary grid CFD algorithm for configuration aerodynamics analysis

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“An arbitrary grid CFD algorithm for configuration aerodynamics analysis” Metadata:

  • Title: ➤  An arbitrary grid CFD algorithm for configuration aerodynamics analysis
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - Computational Mechanics Corp. - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Washington, DC - Knoxville, TN - Springfield, Va

“An arbitrary grid CFD algorithm for configuration aerodynamics analysis” Subjects and Themes:

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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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    YJ-20

    hypersonic anti-ship aeroballistic missile, featuring biconic aerodynamic configuration. The missile was first observed during the preparation of the

    Chengdu J-20

    (January 2001). A Research on the Aerodynamic Characteristics of a Small Aspect Ratio, High Lift Fighter Configuration. Strategic Study of CAE (Report)

    Wing configuration

    Aircraft may have additional minor aerodynamic surfaces. Some of these are treated as part of the overall wing configuration: Winglet: a small fin at the wingtip

    Pusher configuration

    In aeronautical and naval engineering, pusher configuration is the term used to describe a drivetrain of air- or watercraft with propulsion device(s)

    Sukhoi Su-30MKA

    cockpit, radar compartments and the avionics bay. The Su-30MKA aerodynamic configuration is a longitudinal triplane with relaxed stability. The canard

    Sukhoi Su-30

    air superiority fighter and as a strike fighter. The integrated aerodynamic configuration, combined with the thrust vectoring control ability, results in

    Formula One car

    and is determined by the aerodynamic configuration of the car in balancing between high straight-line speed (low aerodynamic drag) and high cornering

    Airbus A350

    low- and high-speed windtunnel testing to refine the aerodynamic design. The final configuration of wing and winglet was achieved for the "Maturity Gate

    PZL-230 Skorpion

    to the aircraft's chief designer, Andrzej Frydrychewicz, the aerodynamic configuration of the Skorpion, with the exception of the tail, had been frozen

    Long Range – Anti Ship Missile (India)

    speeds between Mach 8 to 29. The 2020 test of HSTDV validated aerodynamic configuration of vehicle, ignition and sustained combustion of scramjet engine