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Computing Aerodynamics Of PropfansCost and duration of wind-tunnel tests reduced. Computer program developed to predict interference of slipstream of propfan on supercritical wing at subsonic speeds. Use of program reduces cost and time involved in wind-tunnel testing of newly-designed wing/nacelle configurations. Program written in FORTRAN V.
Document ID
19870000548
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Chandrasekaran, B. (Vigyan Research Associates, Inc.)
Date Acquired
August 13, 2013
Publication Date
November 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 10
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LAR-13623
Accession Number
87B10548
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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