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Wing Tip Vortex DragOptimization of L/D through minimizing induced drag through a detailed flow study together with force, pressure and vorticity measurements is considered. Flow visualization with neutral helium bubbles provides an excellent means of observing the effects of configuration changes.
Document ID
19760003925
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Muirhead, V. U. (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
Aerodynamics
Accession Number
76N11013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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