Object of paper is to review all interference corrections appropriate to tunnel of octagonal section or where they do not exist, to deduce them; effect of tunnel boundaries on angle of incidence, drag, downwash, tailsetting to trim and maximum lift of wing of finite span is deduced and then wings which extend right across tunnel are considered.
Interference on wings, bodies and airscrews in closed tunnel of octagonal section
Australian Council Aeronautics -- Report
1944
26 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Wind tunnel interference on wings, bodies and airscrews
SLUB | 1933
|Wind tunnel interference on wings, bodies and airscrews
TIBKAT | 1933
|Wind Tunnel Interference on Wings, Bodies and Airscrews
NTIS | 1933
|Interference between bodies and airscrews
SLUB | 1934
|Interference between bodies and airscrews
TIBKAT | 1932
|