THE strain energy (UF) in a frame is expressed by the equation
Matrix Analysis of the Circular Conical Fuselage
A Development and Revision of an Earlier Paper to Include the case of Cut-outs
Aircraft Engineering and Aerospace Technology ; 29 , 2 ; 47-55
1957-02-01
9 pages
Article (Journal)
Electronic Resource
English
Matrix Analysis of the Circular Conical Fuselage
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