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  2. Aerodynamic force - Wikipedia

    en.wikipedia.org/wiki/Aerodynamic_force

    There are two causes of aerodynamic force: [1]: §4.10 [2] [3]: 29 . the normal force due to the pressure on the surface of the body; the shear force due to the viscosity of the gas, also known as skin friction.

  3. Zero-lift drag coefficient - Wikipedia

    en.wikipedia.org/wiki/Zero-lift_drag_coefficient

    As noted earlier, , =,. The total drag coefficient can be estimated as: = [()], where is the propulsive efficiency, P is engine power in horsepower, sea-level air density in slugs/cubic foot, is the atmospheric density ratio for an altitude other than sea level, S is the aircraft's wing area in square feet, and V is the aircraft's speed in miles per hour.

  4. Kline–Fogleman airfoil - Wikipedia

    en.wikipedia.org/wiki/Kline–Fogleman_airfoil

    The KF airfoil was designed by Richard Kline and Floyd Fogleman. Aircraft wing showing the KFm4 Step. In the early 1960s, Richard Kline wanted to make a paper airplane that could handle strong winds, climb high, level off by itself and then enter a long downwards glide.

  5. Vortex lattice method - Wikipedia

    en.wikipedia.org/wiki/Vortex_lattice_method

    Simulation of an airplane using Open VOGEL, an open source framework for aerodynamic simulations based in the UVLM. The Vortex lattice method, (VLM), is a numerical method used in computational fluid dynamics, mainly in the early stages of aircraft design and in aerodynamic education at university level.

  6. Area rule - Wikipedia

    en.wikipedia.org/wiki/Area_rule

    The Whitcomb Area Rule: NACA Aerodynamics Research and Innovation, History Nasa. Whitcomb, Richard T. (January 1956). A Study of the Zero-Lift Drag-Rise Characteristics of Wing-Body Combinations Near the Speed of Sound (Technical report). National Advisory Committee for Aeronautics. hdl: 2060/19930092271 – via NASA Technical Reports Server.

  7. Supersonic airfoils - Wikipedia

    en.wikipedia.org/wiki/Supersonic_airfoils

    Years of research and experience with the unusual conditions of supersonic flow have led to some interesting conclusions about airfoil design. Considering a rectangular wing, the pressure at a point P with coordinates (x,y) on the wing is defined only by the pressure disturbances originated at points within the upstream Mach cone emanating from point P. [3] As result, the wing tips modify the ...

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  9. The Flying Circus of Physics - Wikipedia

    en.wikipedia.org/wiki/The_Flying_Circus_of_Physics

    2.3 Aerodynamics of passing trains 2.4 Collapse of the old Tacoma Narrows Bridge 2.5 Aerodynamics of buildings 2.6 Kites 2.7 Ski Jumping 2.8 Speed of a downhill skier 2.9 Boomerangs 2.10 Throwing cards 2.11 Seeds that spin 2.12 Flying snakes 2.13 Air drag on tennis balls 2.14 Veering a football around a defensive wall 2.15 Golf-ball aerodynamics