Because skin of airplane in flight is subjected to combination of stress, attention is given to problem of plate buckling when more than one stress is acting. (Originally issued as Advance Restricted Report L6A05a Mar 1946)
Critical combinations of longitudinal and transverse direct stress for infinitely long flat plate with edges elastically restrained against rotation
Nat Advisory Committee Aeronautics -- Wartime Report
1947
14 pages
6 Supplementary plates
Report
English
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Engineering Index Backfile | 1946
|Vibration analysis of orthotropic Mindlin plates with edges elastically restrained against rotation
Online Contents | 1993
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