Supplementary developments and revisions of two-dimensional airfoil theory; general theorem is proved that in any case of several airfoils with mutual interference, lift force follows same laws in its dependency on angle of attack as in case of single wing. Before Inst Aeronautical Sciences.
New developments in theory of airfoils of infinite span
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 7 , n 7
1940
5 pages
Bibliography
Article (Journal)
English
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On theory of oscillating airfoils of finite span in subsonic compressible flow
Engineering Index Backfile | 1949
|Flow phenomena on plates and airfoils of short span
TIBKAT | 1936
|Extension of theory of oscillating airfoils of finite span in subsonic compressible flow
Engineering Index Backfile | 1951
|