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Source: The Open Library

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12-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall

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“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:

  • Title: ➤  2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
  • Author:
  • Language: English
  • Number of Pages: Median: 559
  • Publisher: ➤  National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
  • Publish Date:
  • Publish Location: ➤  Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va

“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” 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

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    2Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations

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    “Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations” Metadata:

    • Title: ➤  Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations
    • Author:
    • Publisher: ➤  Dept. of Aerospace Science and Engineering - Institute for Aerospace Studies
    • Publish Date:
    • Publish Location: [Downsview, Ont.]

    “Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1979
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    3Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing

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    “Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing” Metadata:

    • Title: ➤  Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing
    • Author:
    • Number of Pages: Median: 23
    • Publisher: National Aerospace Laboratory
    • Publish Date:
    • Publish Location: Tokyo

    “Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1988
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    4Oscillating behaviour of a 7.5% circular arc airfoil

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    “Oscillating behaviour of a 7.5% circular arc airfoil” Metadata:

    • Title: ➤  Oscillating behaviour of a 7.5% circular arc airfoil
    • Author:
    • Publisher: ➤  Dept. of Aerospace Science and Engineering
    • Publish Date:
    • Publish Location: [Downsview, Ont.]

    “Oscillating behaviour of a 7.5% circular arc airfoil” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1987
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    Wiki

    Source: Wikipedia

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    Stall (fluid dynamics)

    fixed-wing aircraft. The principles of stall discussed here translate to foils in other fluids as well. A stall is a condition in aerodynamics and aviation

    Oscillation

    example, the phenomenon of flutter in aerodynamics occurs when an arbitrarily small displacement of an aircraft wing (from its equilibrium) results in an

    Lift (force)

    "The Aerodynamics of Sail Interaction" (PDF). Archived from the original (PDF) on July 7, 2011. Retrieved July 12, 2011. One explanation of how a wing .

    Aeroelasticity

    Aeroelasticity problems can be prevented by adjusting the mass, stiffness or aerodynamics of structures which can be determined and verified through the use of

    Fixed-wing aircraft

    from rotary-wing aircraft (in which a rotor mounted on a spinning shaft generates lift), and ornithopters (in which the wings oscillate to generate lift)

    Insect flight

    attached directly to the wings. In other winged insects, flight muscles attach to the thorax, which make it oscillate in order to induce the wings to beat

    Ornithopter

    D. DeLaurier, "An Overview of Micro Air Vehicle Aerodynamics", Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications, Paul Zarchan

    Kármán vortex street

    Ratio of inertial to viscous forces acting on a liquid Vortex shedding – Oscillating flow effect resulting from fluid passing over a blunt body Vortex-induced

    Vortex

    Effect in physics Strouhal number – Dimensionless number describing oscillating flow mechanisms Vortex engine – Alternative to tall chimneys Vortex tube –

    Tailplane

    rotates around the centre of gravity. For example, when the aircraft is oscillating, but is momentarily aligned with the overall vehicle's motion, the tailplane