NASA NTRS · 19830000079
Wing Subsonic Aerodynamic Performance Estimates
Abstract
Solution by iteration estimates performance of twisted and cambered wings of arbitrary planform. SUBAER based on linearized theory lifting-surface solution provides spanwise distribution of theoretical leading edge thrust, in addition to surface distribution of perturbation velocities. Program written in FORTRAN IV.
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Carlson, H. W., Walkley, K. B.. 1983-08-01. Wing Subsonic Aerodynamic Performance Estimates. https://ntrs.nasa.gov/citations/19830000079
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