NASA NTRS · 19860000338
Wing-Design Program for Subsonic or Supersonic Speeds
Abstract
Surface of mildest possible camber generated. WINGDES provides analysis, design capability and is applicable to both subsonic and supersonic flows. Optimization carried out for entire wing or for designated leading- and trailing-edge areas, for design of missionadaptive surfaces. WINGDES written in FORTRAN IV.
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Carlson, H. W., Walkley, K. B.. 1986-07-01. Wing-Design Program for Subsonic or Supersonic Speeds. https://ntrs.nasa.gov/citations/19860000338
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