In order to provide information for flutter and dynamic stress calculations on aircraft, knowledge of normal modes of vibration is required; matrix method, due to Dr. TRAILL-NASH, is extended and used to obtain general expression for complete aircraft normal modes, and is applicable to most aircraft configurations; method is considered eminently suitable for use with modern digital electronic computational equipment.
Normal modes of vibration of aircraft
Aircraft Eng
Aircraft Engineering ; 25 , n 298
1953
7 pages
Article (Journal)
English
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