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)
Helicopters -- Calculation and design
NASA -- Technical Translation
1968
470 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.