Correction factors for ideal angle of attack and camber due to loading are presented for 3 Bladed 0.2R hub propellers.

    The factors are based on propeller lifting surface theory. Correction factors for ideal angle of attack due to thickness are not included. The propellers are optimum free-running propellers with chordwise loadings identical to NACA a = 0.8 meanline.


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    Title :

    Lifting surface corrections for 3 bladed optimum propellers


    Contributors:

    Published in:

    Publication date :

    1971-12-01


    Size :

    16 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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