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The compressibility rule for drag of airfoil nosesIt is shown that the drag of any semi-infinite airfoil section in purely subsonic inviscid flow follows precisely the Prandtl-Glauert compressibility rule. The result for the parabola has application to leading edge corrections in thin airfoil theory.
Document ID
19760012012
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jones, R. T. (NASA Ames Research Center Moffett Field, CA, United States)
Vandyke, M. D. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 8, 2013
Publication Date
February 1, 1976
Publication Information
Publication: Collected Works of Robert T. Jones
Subject Category
Aerodynamics
Accession Number
76N19100
Distribution Limits
Public
Copyright
Public Use Permitted.
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