Charts are presented from which 24S-T (bare sheet) and 75S-T (Alclad sheet) aluminum alloy flat compression panels may be designed to have minimum weight required to carry given intensity of loading at given effective length of panel with given sheet thickness.
Design charts for flat compression panels having longitudinal extruded Y-section stiffeners and comparison with panels having formed Z-section stiffeners
Nat Advisory Committee Aeronautics -- Tech Note
1947
41 pages
35 Supp sheets
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.