Three-Dimensional, Compressible, Laminar Boundary-Layer Method for GeneralFuselages. Volume 2: User's Manual

摘要

This user's manual contains a complete description of the computer programsdeveloped to calculate three-dimensional, compressible, laminar boundary layers for perfect gas flow on general fuselage shapes. These programs include the 3-D boundary layer program (3DBLC), the body-oriented coordinate program (BCC), and the streamline coordinate program (SCC). Subroutine description, input, output and sample case are discussed. The complete FORTRAN listings of the computer programs are given.