An Improved Panel Method for the Solution of Three-Dimensional Leadingedge Vortex Flows. Volume 2:User's Guide and Programmer's Document.

摘要

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.