By means of integral method, solution is obtained to problem involving gas phase chemical reactions in hypersonic laminar boundary layer; numerical examples show that dissociative equilibrium is not usually reached over plates of reasonable length.
Dissociative relaxation of oxygen over adiabatic flat plate at hypersonic mach numbers
NASA -- Tech Note
1960
28 pages
Report
English
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Transition measurements at hypersonic Mach numbers.
NTRS | 1967
|Transition measurements at hypersonic Mach numbers.
AIAA | 1967
|