NASA NTRS · 19860064271
Application of the TranAir full-potential code to complete configurations
Abstract
The 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.
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Erickson, L. L., Madson, M. D., Woo, A. C.. 1986-01-01. Application of the TranAir full-potential code to complete configurations. https://ntrs.nasa.gov/citations/19860064271
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