Effect of curvatures on strength of axially loaded sheet-stringer panels /
Compressive tests were made on twenty-one 24S-T aluminum-alloy sheet-stringer panels 12 inches in length and 16 inches in developed width, reinforced by four Z stringers spaced 4 inches apart. The radii of curvature R ranged from 19 inches to infinity, the sheet thicknesses at t from 0.025 to 0.190...
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1944
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
944 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 944 |
|---|