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Design procedure for low-drag subsonic airfoilsAirfoil has least amount of drag under given restrictions of boundary layer transition position, lift coefficient, thickness ratio, and Reynolds number based on airfoil chord. It is suitable for use as wing and propeller aircraft sections operating at subsonic speeds and for hydrofoil sections and blades for fans, compressors, turbines, and windmills.
Document ID
19750000256
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Peterson, J. B. (National Res. Council)
Chen, A. B.
Date Acquired
August 8, 2013
Publication Date
October 1, 1975
Subject Category
Physical Sciences
Report/Patent Number
LAR-11351
Report Number: LAR-11351
Accession Number
75B10256
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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