A Theoretical Investigation Of The Aerodynamics Of Slender Wing Body Combinations Exhibiting Leading Edge Separation
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Author | : Alvin H. Sacks |
Publisher | : |
Total Pages | : 124 |
Release | : 1967 |
Genre | : Aerodynamic load |
ISBN | : |
A theoretical analysis is presented for calculating the normal force and center of pressure on plane wing/body combinations exhibiting leading edge separation. The mathematical model for the separated flow involves the shedding of a number of discrete vortex pairs along the wing leading edge, each pair satisfying the Kutta condition at the position of shedding. The subsequent lateral positions of these vortex filaments are calculated step by step, so that the rolling up of the vortex sheet is taken into account. Hence, the method predicts the chordwise normal-force distributions as well as the vortex sheet shapes over the configuration.
Author | : |
Publisher | : |
Total Pages | : 478 |
Release | : 1973 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 868 |
Release | : 1975 |
Genre | : Aerodynamics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 910 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : |
Release | : 1969 |
Genre | : Government publications |
ISBN | : |
Author | : M.Y. Hussaini |
Publisher | : Springer Science & Business Media |
Total Pages | : 367 |
Release | : 2013-06-29 |
Genre | : Science |
ISBN | : 1461246784 |
From the astrophysical scale of a swirling spiral galaxy, through the geophysical scale of a hurricane, down to the subatomic scale of elementary particles, vortical motion and vortex dynamics have played a profound role in our understanding of the physical world. Kuchemann referred to vortex dynamics as "the sinews and muscles of fluid motion. " In order to update our understanding of vortex dominated flows, NASA Langley Research Center and the Institute for Computer Applications in Science and Engineering (ICASE) conducted a workshop during July 9-11, 1985. The subject was broadly divided into five overlapping topics vortex dynamics, vortex breakdown, massive separation, vortex shedding from sharp leading edges and conically separated flows. Some of the experts in each of these areas were invited to provide an overview of the subject. This volume is the proceedings of the workshop and contains the latest, theoretical, numerical, and experimental work in the above-mentioned areas. Leibovich, Widnall, Moore and Sirovich discussed topics on the fundamentals of vortex dynamics, while Keller and Hafez treated the problem of vortex break down phenomena; the contributions of Smith, Davis and LeBalleur were in the area of massive separation and inviscid-viscous interactions, while those of Cheng, Hoeijmakers and Munnan dealt with sharp-leading-edge vortex flows; and Fiddes and Marconi represented the category of conical separated flows.
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 448 |
Release | : 1968 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 436 |
Release | : 1968 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 902 |
Release | : 1978 |
Genre | : Aeronautics |
ISBN | : |
Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.
Author | : H. W. M. Hoeijmakers |
Publisher | : |
Total Pages | : 212 |
Release | : 1989 |
Genre | : Vortex-motion |
ISBN | : |