Report deals with geometrical tunnel configuration hither to unexplored -- namely, tunnel of circular cross section; in addition to finding upwash correction at wing itself, upwash is calculated at various tail positions downstream of wing.
Upwash correction for oscillating wing in wind tunnel
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 20 , n 6 ; p 383-386 + 406
1953
Aufsatz (Zeitschrift)
Englisch
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