Experimental study of deformation and of effective width in axially loaded sheet-stringer panels
The deformation of two sheet-stringer panels subjected to end compression under carefully controlled end conditions was measured at a number of points and at a number of loads, most of which were above the load at which the sheet had begun to buckle. The two panels were identical except for the shee...
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Main Authors: | , , |
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Format: | eBook |
Language: | English |
Published: |
Washington [D.C.] :
National Advisory Committee for Aeronautics,
1939.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
684. |
Subjects: | |
ISBN: | 9781680156027 1680156020 |
Physical Description: | 1 online resource (60 pages, 47 unnumbered pages) : illustrations |
Online Access:
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