Vibrations and dynamic stability; current methods of calculating elastic vibrations of blade, performed on high-speed electronic computers which permits determining variable stresses set up in blade; problem of vibrations of helicopter parts, examined from viewpoint of crew and passenger comfort; calculation of special bearings necessary in designing many helicopter components; economic considerations of aviation engineering of importance in designing, are also presented; discussion of problems of balancing, controllability, and stability from viewpoint of selecting parameters for control system. Translated from " Mashinostroyeniye" Press Moscow, 1967. (11448)


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    Title :

    Helicopters -- Calculation and design


    Additional title:

    NASA -- Technical Translation


    Contributors:
    Mil', M.L. (author)

    Published in:

    Publication date :

    1968


    Size :

    470 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Helicopters Calculation and Design. Volume I - Aerodynamics

    A. S. Braverman / L. N. Grodko / M. A. Leykand et al. | NTIS | 1967


    Helicopters: Calculation and Design. Vibrations and Dynamic Stability

    M. L. Mil / A. V. Nekrasov / A. S. Braveman et al. | NTIS | 1968



    Helicopters and aeroplane-helicopters

    Lame´ / M. | Engineering Index Backfile | 1921


    Design of small helicopters

    Payne, P.R. | Engineering Index Backfile | 1955