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A study of three-dimensional interaction of wakes and boundary-layersYeung, Chong Pui January 1993 (has links)
No description available.
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An experimental investigation into the use of vortex generators to improve the performance of a high lift systemInnes, Fraser January 1995 (has links)
No description available.
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An investigation into the aerodynamics of Gurney flapsJeffrey, David Robert Michael January 1998 (has links)
No description available.
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Multigrid multiblock computation of steady compressible flowsAves, Mark Antony January 1991 (has links)
No description available.
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Calculation of the pressure distribution on a pitching airfoil with application to the Darrieus RotorGhodoosian, Nader 28 September 1983 (has links)
An analytical model leading to the pressure distribution on
the cross section of a Darrieus Rotor Blade (airfoil) was constructed. The model was based on the inviscid flow theory and the contribution of the nonsteady wake vortices was neglected. The
analytical model was translated into a computer code in order to
study a variety of boundary conditions encountered by the rotating
blades of the Darrieus Rotor.
The results of the program indicate that for a pitching airfoil, lift can be adequately approximated by the Kutta-Joukowski forces, despite notable deviations in the pressure distribution on
the airfoil. These deviations are most significant at the upwind
half of the Darrieus Rotor where higher lift is accompanied by
increased adverse pressure gradients. It was also found that the effect of pitching on lift can be approximated by a linear shift in
the angle of attack proportional to the blade angular velocity.
Finally, the fluid velocity about the pitching-only NACA 0015
was tabulated; thus allowing the principle of superposition to be
used in order to determine the fluid velocity about a translating
and pitching airfoil. / Graduation date: 1984
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Experiment on flow-induced vibration of an airfoil due to vortex shedding generated from upstream circular cylinder /Luk, K. F. January 2002 (has links)
Thesis (M. Phil.)--Hong Kong University of Science and Technology, 2002. / Includes bibliographical references (leaves 54-57). Also available in electronic version. Access restricted to campus users.
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Doppler global velocimetry measurements in a wing flow field with tip blowingStarn, Andrew Douglas. January 2004 (has links)
Thesis (M.S.)--West Virginia University, 2004. / Title from document title page. Document formatted into pages; contains vi, 101 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 41-45).
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Boundary-layer separation and control /Atik, Hediye, January 2002 (has links)
Thesis (Ph. D.)--Lehigh University, 2003. / Includes vita. Includes bibliographical references (leaves 264-274).
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A hybrid inverse optimization method for aerodynamic design of lifting surfacesSantos, Luis Carlos de Castro 05 1900 (has links)
No description available.
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The investigation of two subsonic type airfoils in the transonic region by application of the hydraulic analogyDansby, Ted 12 1900 (has links)
No description available.
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