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.


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    Title :

    Heat transfer to cylinders in crossflow in hypersonic rarefied gas streams


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Heat transfer to cylinders in crossflow in hypersonic rarefied gas streams

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