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Experimental Test Of Aerodynamic Computer ProgramLinear potential-flow theory applied to advanced airplane design. Report discusses use of PANAIR computer program to predict airflow about advanced fighter aircraft. Predictions compared with measurements about scale model of aircraft in wind tunnel at mach numbers of 0.6, 0.9, and 1.2 and at angles-of-attack from 0 to 10 degree.
Document ID
19880000123
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Madson, M. D. (NASA Ames Research Center, Moffett Field, Calif.)
Erickson, L. L. (NASA Ames Research Center, Moffett Field, Calif.)
Date Acquired
August 13, 2013
Publication Date
February 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11733
ISSN: 0145-319X
Report Number: ARC-11733
Accession Number
88B10123
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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