Results indicate that partial-power vertical descents and landing approaches produce rotor blade moments that are higher than moments encountered in any other flight condition investigated.


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    Title :

    Flight investigation of effects of transition, landing approaches. Partial-power vertical descents, and droop-stop pounding on bending and torsional moments encountered by helicopter rotor blade


    Additional title:

    NASA -- Memo


    Contributors:
    Ludi, L.H. (author)

    Published in:

    Publication date :

    1959


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :