On the Gradient Functions for Nonequilibrium Dissociative Flow Behind a Shock

• 1 April 1961
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
• Vol. 28  (4) , 337-339
• https://doi.org/10.2514/8.8975

Abstract

Keywords

• GRADIENT FUNCTIONS
• SHOCK
• NONEQUILIBRIUM DISSOCIATIVE FLOW