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Application of the TranAir full-potential code to complete configurationsThe TranAir computer code solves the full-potential equation for transonic flow by combining a rectangular box of flow-field grid points with networks of surface panels. Complex geometry is easily represented since surface conforming flow-field grids are not used. Application of TranAir to the F-16A is presented for free-stream Mach numbers of 0.6 and 0.90, at an angle of attack of four degrees.
Document ID
19860064271
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Erickson, L. L. (NASA Ames Research Center Moffett Field, CA, United States)
Madson, M. D. (NASA Ames Research Center Moffett Field, CA, United States)
Woo, A. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Accession Number
86A49009
Funding Number(s)
CONTRACT_GRANT: NAS2-11851
Distribution Limits
Public
Copyright
Other

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