Accession Number : AD0155834

Title :   Cyclic Creep Buckling of Integrally Stiffened Aluminum Alloy Panels.

Corporate Author : NORTH AMERICAN AVIATION INC LOS ANGELES CALIF

Personal Author(s) : King,C. W. ; Nolan,B. J.

Report Date : APR 1958

Pagination or Media Count : 110

Descriptors :   *AIRPLANE PANELS, *ALUMINUM ALLOYS, BUCKLING, CREEP, STRESSES, TEMPERATURE

Distribution Statement : APPROVED FOR PUBLIC RELEASE