Accession Number:

AD0155834

Title:

Cyclic Creep Buckling of Integrally Stiffened Aluminum Alloy Panels.

Personal Author(s):

Corporate Author:

NORTH AMERICAN AVIATION INC LOS ANGELES CALIF

Report Date:

1958-04-01

Supplementary Note:

Rept. on Structural Design Criteria.

Pages:

0110

Descriptors:

Contract Number:

AF33 616 3369

File Size:

0.00MB

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