Theory applicable to swept wings for all useful frequencies of oscillation, but restricted to straight trailing edges and to aspect ratios less than 4; results are in accord with Garrick theory for plan forms of very low aspect ratio and with infinite aspect ratio theory for rectangular wings.
Aerodynamic forces on low aspect ratio wings oscillating in incompressible flow
J. Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 11
1952
13 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Aerodynamic forces on rectangular wings oscillating in subsonic flow
Engineering Index Backfile | 1960
|