Investigation of effect of bluntness on two-dimensional hypersonic inlet type flows; tests were performed on two geometric configurations -- flat plate and isentropic compression ramp -- each accommodating leading edges of three different radii; results are compared with theoretical analyses and reflect blunt leading-edge effects on inviscid-flow profiles, surface-pressure phenomena and viscous-layer growth along models, with and without incident shock wave-boundary layer interactions. (09561)
Effect of bluntness on hypersonic two-dimensional inlet type flows
NASA CR
NASA Contractor Reports ; n 1145
1968
91 pages
Report
Englisch
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