Study to determine spanwise distribution of lift increase due to slipstream at different angles of attack of wing and at different free stream to slipstream velocity ratios; empirical evaluation of destalling effects made for STOL configuration of experiment.
Experimental investigation of aerodynamics of wing in slipstream
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 25 , n 5
1958
5 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Aerodynamics of wing-slipstream interaction : a numerical study
TIBKAT | 1971
|Effect of slipstream on airplane wing
Engineering Index Backfile | 1939
|Analysis of Wing Slipstream Flow Interaction
NTIS | 1970
|