The results of an analytical study of aerodynamic interference effects for a light twin aircraft are presented. The data presented concentrates on the influence of a wing on a body (the fuselage). Wind tunnel comparisons of three fillets are included, with corresponding computational analysis. Results indicate that potential flow analysis is useful to guide the design of intersection fairings, but experimental tuning is still required. While the study specifically addresses a light twin aircraft, the methods are applicable to a wide variety of aircraft.
Studies of Light-Twin Wing-Body Interference
Sae Technical Papers
Business Aircraft Meeting and Exposition ; 1983
01.02.1983
Aufsatz (Konferenz)
Englisch
Aerodynamics , Fairings , Aircraft , Fuselages , Wings , Wind tunnel tests
Studies of light-twin wing-body interference
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