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Drag reduction through higher wing loadingA reduction in wing area, thickness, and span increases wing loading and lowers parasitic drag for a typical light airplane by 10.5%.
Document ID
19760003921
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kohlman, D. L. (Kansas Univ. Lawrence, KS, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Proc. of the NASA, Ind., Univ., Gen. Aviation Drag Reduction Workshop
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N11009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19760003909Collected WorksProceedings of the NASA, Industry, University, General Aviation Drag Reduction Workshop
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