Accession Number:

ADA801560

Title:

Compressive Strength of Flat Panels with Z-Section Stiffeners

Corporate Author:

NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS LANGLEY FIELD VA LANGLEY AERONAUTICAL LABORATORY

Report Date:

1944-02-01

Abstract:

Compression tests were made on several series of flat panels with Z-section stiffeners, in which relative dimensions were varied individually. The test data presented show the effect of each dimension ratio on the buckling stress for the sheet and on the average stress at maximum load.

Descriptive Note:

Wartime rept.

Pages:

0020

Identifiers:

Modernization Areas:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

9.71MB