Image system required to satisfy boundary conditions for wing body combination in closed circular tunnel is deduced, and upwash interference due to tunnel wall is thereby calculated; development starts from first principles and utilizes elementary methods; results indicate interference significantly different from that obtained for wing alone.
Wind-tunnel wall corrections for wing-body combinations
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 16 , n 4
1949
6 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
NTRS | 1948
|Tema Archiv | 1996
|Subsonic wind tunnel wall corrections
TIBKAT | 1966
|Subsonic Wind Tunnel Wall Corrections
NTIS | 1966
|Engineering Index Backfile | 1958
|