NASA NTRS · 19830000395
Transonic Airfoil Analysis
Abstract
Program uses fast iteration scheme for solving transonic flow field around arbitrary airfoils. Transonic Airfoil Analysis Computer Code, TAIR, employs fast, fully implicit algorithm to solve conservative full-potiential equation for steady transonic flow field about arbitrary airfoil immersed in subsonic free stream. TAIR written in FORTRAN IV.
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Holst, T. L., Dougherty, F. C., Gundy, K. L., Thomas, S. D., Frick, J., Fernquist, A., Albert, J.. 1984-04-01. Transonic Airfoil Analysis. https://ntrs.nasa.gov/citations/19830000395
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