Turbulent flow measurement of frictional resistance of three smooth plank surfaces, of lengths 50 ft, 18 ft, and 10 ft; new formulas given for width of friction belt and for velocity distribution within belt; predicated on data, method of correcting for wake scale effect in estimating ship powers and propeller revolutions from self propelled model results. (See also - discussion pt 7 May-June p D65-78, supp table)


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    Title :

    Wake studies of plane surfaces


    Additional title:

    North East Coast Instn Engrs Shipbldrs -- Trans


    Contributors:
    Allan, J.F. (author) / Cutland, R.S. (author)


    Publication date :

    1953


    Size :

    22 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Hypersonic Range Wake Studies

    L. Sevigny / L. Tardif / J. G. G. Dionne et al. | NTIS | 1971


    Passive pressure-drag control in a plane wake

    GRINSTEIN, F. F. / BORIS, J. P. / GRIFFIN, O. M. | AIAA | 1991


    Simulations of high-frequency excitation of a plane wake

    Cain, Alan / Rogers, Michael / Kibens, Valdis | AIAA | 2001


    Wake-Vortex Alleviation Flowfield Studies

    Durston, D.A. | Online Contents | 2005


    Subsonic Axisymmetric Near-Wake Studies

    R. A. Merz / R. H. Page / C. E. G. Przirernbel | AIAA | 1978