Formulas designed to estimate blade root thickness on basis of assumed acceptable working stresses; values derived by method will approximate thicknesses determined from more detailed considerations; while formulas are not suggested as substitute for more complete analysis, they provide method of assuming suitable stress and solving quickly for blade thickness; accuracy is sufficient to enable preliminary estimates of propeller weights.


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    Title :

    Estimating propeller blade thickness


    Additional title:

    Mar Eng


    Contributors:
    Baier, L.A. (author)

    Published in:

    Publication date :

    1959


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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