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
Conference paper
English
© Metadata Copyright Elsevier B. V. All rights reserved.
SECONDARY FATIGUE LOADING OF HELICOPTERS
SAE Technical Papers | 1954
|Engineering Index Backfile | 1952
|Loading Spectra, Usage Monitoring and Prediction of Fatigue Damage in Helicopters
British Library Conference Proceedings | 1995
|Fatigue of helicopters : Tests and calculations
TIBKAT | 1965
|Airworthiness requirements and fatigue of helicopters
Engineering Index Backfile | 1951
|