Results indicate that maximum moments encountered in partial power descents with forward speed tend to be reduced from maximum moments encountered during partial power descents at zero forward speed; large torsional moments were found to occur during high speed level turns and pullouts from autorotation.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Investigation of effects of selected operating conditions on bending and torsional moments encountered by helicopter rotor blade


    Additional title:

    NASA -- Tech Note


    Contributors:
    Ludi, L.H. (author)


    Publication date :

    1961


    Size :

    43 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :