درباره ما
NACA-TR-636
Approximate Stress Analysis of Multistringer Beams with Shear Deformation of the Flanges
Year: 1938
Abstract: The problem of the skin-stringer combinations used as axially loaded panels or as covers for box beams is considered from the point of view of the practical stress analyst. By a simple substitution the problem is reduced to the problem of the single-stringer structure, which has been treated in NACA Report no. 608. The method of making this substitution is essentially empirical; in order to justify it, comparisons are shown between calculations and strain-gage tests of three beams tested by the author and of one compression panel and three beams tested and reported elsewhere.
Subject: AIRCRAFT STRUCTURES
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:04:07Z | |
| date available | 2017-09-04T18:04:07Z | |
| date copyright | 01/01/1938 | |
| date issued | 1938 | |
| identifier other | GFYHUEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/187012 | |
| description abstract | The problem of the skin-stringer combinations used as axially loaded panels or as covers for box beams is considered from the point of view of the practical stress analyst. By a simple substitution the problem is reduced to the problem of the single-stringer structure, which has been treated in NACA Report no. 608. The method of making this substitution is essentially empirical; in order to justify it, comparisons are shown between calculations and strain-gage tests of three beams tested by the author and of one compression panel and three beams tested and reported elsewhere. | |
| language | English | |
| title | NACA-TR-636 | num |
| title | Approximate Stress Analysis of Multistringer Beams with Shear Deformation of the Flanges | en |
| type | standard | |
| page | 21 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1938 | |
| contenttype | fulltext | |
| subject keywords | AIRCRAFT STRUCTURES | |
| subject keywords | AXIAL COMPRESSION LOADS | |
| subject keywords | BEAMS (SUPPORTS) | |
| subject keywords | DEFORMATION | |
| subject keywords | FLANGES | |
| subject keywords | FORMULAS | |
| subject keywords | NUMERICAL ANALYSIS | |
| subject keywords | RIBS (SUPPORTS) | |
| subject keywords | SHEAR STRESS | |
| subject keywords | STRESS ANALYSIS | |
| subject keywords | STRESSED-SKIN STRUCTURES | |
| subject keywords | STRINGERS | |
| subject keywords | WINGS |