NASA NTRS · 19800018781
An improved panel method for the solution of three-dimensional leading edge vortex flows Volume 2: User's guide and programmer's document
Abstract
A computer program developed for solving the subsonic, three dimensional flow over wing-body configurations with leading edge vortex separation is presented. Instructions are given for the proper set up and input of a problem into the computer code. Program input formats and output are described, as well as the overlay structure of the program. The program is written in FORTRAN.
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Tinoco, E. N., Lu, P., Johnson, F. T.. 1980-07-01. An improved panel method for the solution of three-dimensional leading edge vortex flows Volume 2: User's guide and programmer's document. https://ntrs.nasa.gov/citations/19800018781
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