The fundamentals of oscillation theory and mathematical statistics applicable to problems of the dynamics of aircraft structures and aerodynamic loads on aircraft and missiles during various stages of flight are presented. Data is included on the elasticity of structures in gusts of rough air when taking off and landing, vibrations of aircraft and helicopter parts, and the effect of these parameters on the strength of the structure and the performance of aircraft equipment. An analysis of the structural parameters influencing flutter and the methods used to study flutter characteristics is provided. The fatigue strength of aircraft structures and the basic trends in the use of computers to study the dynamic strength of aircraft structures are reported. (Author)
External Loads and Aircraft Strength
1973
392 pages
Report
Keine Angabe
Englisch
External loads and aircraft strength
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