Drag of Finite-Length Cylinders Determined from Flight Tests at High Reynolds Numbers for Mach Number Range from 0.5 to 1.3.


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    Title :

    Drag of finite-length cylinders determined from flight tests at high Reynolds numbers for mach number range from 0.5 to 1.3


    Additional title:

    NACA -- Tech Note


    Contributors:
    Welsh, C.J. (author)


    Publication date :

    1953


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English