Weight of compression panel subjected to given buckling load investigated as function of stiffener spacing, plate thickness, and geometry of stiffener cross section; charts presented for determination of optimum stiffener spacing and plate thickness.
Minimum-weight design of simply supported transversely stiffened plates under compression
Nat Advisory Committee Aeronautics -- Tech Note
1948
23 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Minimum weight design aspects of stiffened cylinders under compression
Engineering Index Backfile | 1967
|