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book (5)

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English (5)

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1999 (1)

1985 (1)

1982 (1)

1968 (2)

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Book

Application of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings
Authors: Polhamus, Edward C. --- United States. --- Langley Research Center.
Year: 1968 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Keywords
Delta wing airplanes. --- Vortex flaps. --- Drag (Aerodynamics) --- Lift (Aerodynamics)

Book

VORCOR : a computer program for calculating characteristics of wings with edge vortex separation by using a vortex filament and core model
Authors: Pao, Jenn-Louh --- Mehrotra, Sudhir C. --- Lan, C. Edward --- Langley Research Center --- Vigyan Research Associates.
Year: 1982 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Abstract

Keywords
Computer programs. --- Vortex flaps. --- Computerized simulation. --- Aerodynamics. --- Mathematical models.

Book

Application of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings
Authors: Polhamus, Edward C. --- United States. --- Langley Research Center.
Year: 1968 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Abstract

Keywords
Delta wing airplanes. --- Vortex flaps. --- Drag (Aerodynamics) --- Lift (Aerodynamics) --- Delta wing airplanes. --- Drag (Aerodynamics) --- Lift (Aerodynamics) --- Vortex flaps.

Book

Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications
Authors: Hahne, David E. --- Langley Research Center
Year: 1999 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Keywords
Scale models. --- Leading edges. --- Data bases. --- F-16 aircraft. --- Leading edge sweep. --- Vortex flaps.

Book

Calculation of vortex-flap aerodynamic characteristics
Authors: Lan, C. Edward --- Hsing, C. C. --- University of Kansas. --- United States.
Year: 1985 Publisher: Lawrence, Kansas : [Washington, D.C.] : Flight Research Laboratory, Department of Aerospace Engineering, the University of Kansas ; [National Aeronautics and Space Administration],

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Abstract

Keywords
Aerodynamic configurations. --- Angle of attack. --- Leading edges. --- Spline functions. --- Swept wings. --- Vortex breakdown. --- Vortex flaps.

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