Analytical Study of Three-Surface Lifting Systems
Conventional, canard, and three surface aircraft configurations are investigated analytically to determine each configuration's induced drag, as well as the pressure and viscous drag. A vortex panel method in conjunction with momentum integral boundary layer method is used to predict inviscid and viscous characteristics. Vortex lattice methods are used to trim the aircraft as well as to predict the induced drag of each configuration. Viscous and induced drag results are presented for two different payloads, a six-place and a twelve-place configuration. For both payloads the conventional configuration had the highest lift over drag. However, the canard and the three surface were close enough to warrant consideration based on other criteria.
K. Rokhsaz and B. P. Selberg, "Analytical Study of Three-Surface Lifting Systems," SAE Technical Papers, SAE International, Jan 1985.
The definitive version is available at https://doi.org/10.4271/850866
General Aviation Aircraft Meeting and Exposition
Mechanical and Aerospace Engineering
Keywords and Phrases
Aircraft Configurations; Boundary Layer Methods; Induced Drag; Lifting Systems; Momentum Integral; Viscous Drag; Vortex Lattice Method; Vortex-Panel Method; Warrant Consideration
Article - Conference proceedings
© 1985 SAE International, All rights reserved.
01 Jan 1985