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- W758654849 abstract "The results of an analytical and experimental study of aerodynamic interference effects for a light twin aircraft are presented. Both the influence of a body (either fuselage or nacelle) on a wing and the influence of a wing on a body are studied. The wing studied uses a new natural laminar flow airfoil with variable camber movable trailing edge. A three-dimensional panel method program utilizing surface source and surface doublet singularities was used to design wing-nacelle and wing-fuselage fairings. Experiments were conducted using a 1/6 scale reflection plane model. Forces, pressures, and surface flow visualization results are presented. 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 addressed a light twin aircraft, the methods are applicable to a wide variety of aircraft." @default.
- W758654849 created "2016-06-24" @default.
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- W758654849 date "1982-01-01" @default.
- W758654849 modified "2023-09-27" @default.
- W758654849 title "Computational and experimental studies of light twin aerodynamic interference" @default.
- W758654849 hasPublicationYear "1982" @default.
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