THIS paper is intended as a sequel to a paper by Dr. J. F. C. Conn entitled “Vibration of a Truncated Wedge” (AIRCRAFT ENGINEERING, Vol. XVI, April 1944, pp. 103–105). The three modes of vibration—longitudinal, flexural and torsional—of a truncated cone encastré at one end and free at the other are considered separately. Special attention is given to the vibration frequencies of the cone and uniform cylinder.
The Calculation of Frequencies of Vibration of a Truncated Cone
Development of the Theories for the Longitudinal, Flexural and Torsional Vibration of a Truncated Wedge
Aircraft Engineering and Aerospace Technology ; 18 , 7 ; 235-236
1946-07-01
2 pages
Article (Journal)
Electronic Resource
English
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