Analysis presented provides background for program, and data indicating effect of various components on overall drag of model; attention is devoted to drag of various hub-pylon combinations tested, and effect of rotor height above fuselage; conclusions pertaining to performance capabilities of helicopters of light observation category.
Full scale wind tunnel investigation of helicopter drag
Am Helicopter Soc -- J
American Helicopter Society -- Journal ; 6 , n 1
1961
7 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Full-scale wind tunnel investigation of a helicopter individual blade control system
Tema Archiv | 1993
|