Study made for specific application to airplane wing design. (Advance Restricted Report L4H29)
Charts for calculation of critical compressive stress for local instability of idealized web- and T-stiffened panels
Nat Advisory Committee Aeronautics -- Wartime Report
1944
8 pages
6 Supp plates
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Method of calculating compressive strength of Z-stiffened panels that develop local instability
Engineering Index Backfile | 1947
|DESIGN CHARTS for Longitudinally Stiffened Wing Compression Panels
SAE Technical Papers | 1949
|