Contours of temperature for flow over a blunt body as it flies
through the atmosphere at an altitude of 100 km with a speed of 8
km/sec.
Return to Bow Shock Radiation Project
Return to Nonequilibrium
Gas Dynamics Group
Return to Computational Fluid
Dynamics Laboratory
Return to Sibley School
Please direct any questions regarding this server to Haifang Telc.
haifang@mae.cornell.edu