Reverse-flow relations provide convenient expressions for aerodynamic forces which act on general wing-fuselage combination; drag, lift, spanwise and chordwise lift distributions, and wing moments are treated; available methods and results are considered which apply to wing-fuselage interference problem; reverse-flow relations are then employed to effect desirable changes in defining force expressions by introducing wings or fuselages in reverse flow.
Forces on wing-fuselage combinations in supersonic flow
J Fluid Mechanics
Journal of Fluid Mechanics ; 8 , Part 2
1960
17 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Aerodynamic Centre of Wing-Fuselage Combinations
NTIS | 1976
Wing/Fuselage Interferences in Supersonic and Hypersonic Flow
British Library Conference Proceedings | 1993
|