Comparison of heat transfer data for cylinders in crossflow at hypersonic Mach numbers for gases of different specific heat ratio, molecular weight, and accommodation coefficient; data extend into all flow regimes from free-molecule to almost continuum flow; this made it possible to determine approximate transition points from one flow region into another and to obtain accommodation coefficients.
Heat transfer to cylinders in crossflow in hypersonic rarefied gas streams
NASA -- Tech Note
1960
24 pages
Report
English
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