Approximate method for determination of stresses in and deflections of fuselage; methods and formulas outlined are applicable to any shape of fuselage, but elliptical one is assumed. (See also - n 146 Apr 1941 p 90-4)
Tapered spar frames
Aircraft Eng
Aircraft Engineering ; 13 , n 148
1941
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Emerald Group Publishing | 1941
|Emerald Group Publishing | 1941
Stiffness matrix for a tapered spar element
TIBKAT | 1970
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