High temperatures that can develop in aircraft during supersonic flight make it important to consider possible limitations due to creep on useful service life of structural components; analysis indexed in Engineering Index 1952 p 200 from J Aeronautical Sciences July 1952, is extended to solid rectangular section column.
Creep-buckling analysis of rectangular-section columns
NACA -- Tech Note
1953
24 pages
Report
Englisch
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Creep-buckling analysis of rectangular-section columns
NTRS | 1953
|Creep-buckling analysis of rectangular-section columns
TIBKAT | 1953
|Engineering Index Backfile | 1954
|NTIS | 1954
|NTRS | 1954
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