Tests covered range of simulated density altitudes from 4000 to 33,000 ft, of velocities between fins from Mach number of 0.05 to near sonic values, and of heat inputs from 0 to 500 Btu per hr psi of cylinder wall surface. See also Engineering Index 1947 p 34. (released 1948; 20¢)


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    Title :

    Compressibility and heating effects on pressure loss and cooling of baffled cylinder barrel


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1944


    Size :

    22 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English