Abstract
Hypersonics for the foreseeable future is the domain of space access and hypersonic flight. A hypersonic vehicle encounters an aero-thermodynamic environment characterized by strong shocks and high temperatures, and the flow in the hypersonic regime behaves quite differently from that at supersonic Mach numbers (Bertin in Hypersonic Aerothermodynamics. Washington DC, 1994; Park in Nonequilibrium Hypersonic Aerothermodynamics, Wiley, New York, 1989; Anderson in Hypersonic and High Temperature Gas Dynamics. McGraw-Hill Book Company, New York, 1989).
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
