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The Computation of Induced Drag with Nonplanar and Deformed Wakes

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kroo, Ilan, author.
Conference Name:
Aerospace Technology Conference & Exposition (1990-10-01 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1990
Summary:
AbstractThe classical calculation of inviscid drag, based on far-field flow properties, is re-examined with particular attention to the nonlinear effects of wake roll-up. Based on a detailed look at nonlinear, inviscid flow theory, the paper concludes that many of the classical, linear results are more general than might have been expected. Departures from the linear theory are identified and design implications are discussed. Results include the following: Wake deformation has little effect on the induced drag of a single element wing, but introduces first order corrections to the induced drag of a multi-element lifting system. Far-field Trefftz-plane analysis may be used to estimate the induced drag of lifting systems, even when wake roll-up is considered, but numerical difficulties arise. The implications of several other approximations made in lifting line theory are evaluated by comparison with more refined analyses
Notes:
Vendor supplied data
Publisher Number:
901933
Access Restriction:
Restricted for use by site license

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