Evaluation of loads; possible sources for both steady and oscillating loads; air and inertia loads on rotor blades; engine gas torque and inertia loads; fuselage vibratory loads; lack of information on actual values or cyclic loads encountered in helicopters; need for more emphasis on load problem by government procuring and research agencies.
Secondary fatigue loading of helicopters
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1954 Stresses
1954
6 pages
4 Supp plates
Aufsatz (Konferenz)
Englisch
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