Aircraft and missile structural vibration problems, and dynamics problems associated with missile test and launch equipment may be represented ideally by masses interconnected by extensional and rotational springs; method enabling engineer rapidly to set up vibration problems by using electronic computer and by filling primary data into basic matric equation.
Matric formulation of linearly coupled vibration problems
Aircraft Eng
Aircraft Engineering ; 30 , n 353
1958
8 pages
Aufsatz (Zeitschrift)
Englisch
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A Matric Formulation of Linearly Coupled Vibration Problems
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