Publication Date:
2016-06-07
Description:
A three-dimensional boundary-layer code was developed for particular application to realistic hypersonic aircraft. It is very general and can be applied to a wide variety of boundary-layer flows. Laminar, transitional, and fully turbulent flows of compressible, reacting gases are efficiently calculated by use of the code. A body-oriented orthogonal coordinate system is used for the calculation and the user has complete freedom in specifying the coordinate system within the restrictions that one coordinate must be normal to the surface and the three coordinates must be mutually orthogonal.
Keywords:
AERODYNAMICS
Type:
NASA. Langley Res. Center Aerodynamic Analyses Requiring Advanced Computers, Pt. 1; p 77-99
Format:
application/pdf