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
01.02.1957
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Matrix Analysis of the Circular Conical Fuselage
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