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Transonic airfoil design codeProgram aids in design of shockless airfoils, assists development of fuel-conserving, supercritical wings. Algorithm calculates approximate airfoil shape given prescribed pressure distribution. This allows design of families of transonic airfoils for use in aircraft wings or turbine and compressor blades. Program is written in FORTRAN IV for batch execution on CDC-6000.
Document ID
19800000085
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bauer, F. (New York Univ.)
Garabedian, P. (New York Univ.)
Korn, D. (New York Univ.)
Date Acquired
August 10, 2013
Publication Date
August 1, 1980
Publication Information
Publication: NASA Tech Briefs
Volume: 5
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12460
Accession Number
80B10085
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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