Wind tunnel study made at several fineness ratios between 2 and 14 for range of R from 300,000 to 1,650,000; effects of hemispherical ends on drag characteristics were also obtained; data may be useful in making preliminary calculations on rockets and aircraft having long nose sections at high angles of attack.


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    Title :

    Effects of fineness ratio and Reynolds number on low-speed crosswind drag characteristics of circular and modified-square cylinders


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :