Hypersonic, Nonequilibrium Flow Over a Cylindrically Blunted 6 Deg Wedge

By: Nasa, National Aeronautics and Space Adm

The numerical simulation of hypersonic flow in chemical nonequilibrium over cylindrically blunted 6 degree wedge is described. The simulation was executed on a Cray C-90 with Program LAURA 92-vl. Code setup procedures and sample results, including grid refinement studies and variations of species number are discussed. This simulation relates to a study of wing leading edge heating on transatmospheric vehicles. Gnoffo, Peter A. Langley Research Center RTOP 506-40-91-02...

• Format: Paperback
• Language: English
• ISBN: 1728952913
• ISBN13: 9781728952918
• Release Date: January 1
• Publisher: Independently Published
• Length: 42 Pages
• Weight: 0.27 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"