IN this part we shall consider the effect of non-uniformity (with respect to k) in the longitudinal members, with particular reference to the case of four longerons, and we shall then go on to discuss the treatment of cut-outs.
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 , 3 ; 77-88
1957-03-01
12 pages
Article (Journal)
Electronic Resource
English
Matrix Analysis of the Circular Conical Fuselage
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