Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1988-11-17
1991-02-05
Jordan, Charles T.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
F15D 112, H04R 906
Patent
active
049898108
ABSTRACT:
A method and an apparatus for influencing a laminar-turbulent boundary layer transition on bodies in flow is indicated. The disturbances are in this case introduced into the boundary layer in an unsteady manner. The disturbances are induced by blowing-out and sucking-off and/or by oscillations of the surface and/or by sound pressure.
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DFVLR-AIAA-83-1673 Problems Associated with Artificial Boundry Layer Tranion, by H. U. Meier, H. P. Kreplin.
Control of Laminar-Instability Waves Using a New Technique, by H. W. Liepmann, G. L. Brown and D. M. Nosenchuck.
AIAA-89-1005 Boundary Layer Transition Controlled by Flush Mounted Electro Acoustic Generators, by H. U. Meier, DNW & Zhou Ming de Nai.
de Zhou Ming
Maier Alois
Meier Hans U.
Deutsche Forschungs -und Versuchsanstalt fur Luft -und Raumfahrt
Jordan Charles T.
Wendtland Richard W.
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