NASA NTRS · 19880000123
Experimental Test Of Aerodynamic Computer Program
Abstract
Linear 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.
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Madson, M. D., Erickson, L. L.. 1988-02-01. Experimental Test Of Aerodynamic Computer Program. https://ntrs.nasa.gov/citations/19880000123
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