NASA NTRS · 19800007773
Development of panel methods for subsonic analysis and design
Abstract
Two computer programs, developed for subsonic inviscid analysis and design are described. The first solves arbitrary mixed analysis design problems for multielement airfoils in two dimensional flow. The second calculates the pressure distribution for arbitrary lifting or nonlifting three dimensional configurations. In each program, inviscid flow is modelled by using distributed source doublet singularities on configuration surface panels. Numerical formulations and representative solutions are presented for the programs.
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Bristow, D. R.. 1980-02-01. Development of panel methods for subsonic analysis and design. https://ntrs.nasa.gov/citations/19800007773
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