NASA NTRS · 19830000194
Interactive Graphics Analysis for Aircraft Design
Abstract
Program uses higher-order far field drag minimization. Computer program WDES WDEM preliminary aerodynamic design tool for one or two interacting, subsonic lifting surfaces. Subcritical wing design code employs higher-order far-field drag minimization technique. Linearized aerodynamic theory used. Program written in FORTRAN IV.
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Townsend, J. C.. 1983-10-01. Interactive Graphics Analysis for Aircraft Design. https://ntrs.nasa.gov/citations/19830000194
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