درباره ما
NASA-TN-D-402
Analysis of frame-reinforced cylindrical shells. Part III - Applications
Year: 1960
Abstract: There are basically two approaches to determining stresses that are due to concentrated loads applied to flexible frames which are supported by cylindrical shells. One is to make a complete redundant analysis of each problem, utilizing a large digital computer. The second, which is adopted here, is to devise simple approximate procedures. Such procedures should promote a better understanding of the problem, and provide tables or charts of results as functions of as few parameters as practicable. The analysis is undertaken in references 1 and 2. The results obtained from that analysis are summarized in this report which is intended to be a reference for persons interested in using the results, but who are not concerned with the mathematical derivations.
Subject: ANALYSIS
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:54:19Z | |
| date available | 2017-09-04T15:54:19Z | |
| date copyright | 01/01/1960 | |
| date issued | 1960 | |
| identifier other | QRTKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/57611 | |
| description abstract | There are basically two approaches to determining stresses that are due to concentrated loads applied to flexible frames which are supported by cylindrical shells. One is to make a complete redundant analysis of each problem, utilizing a large digital computer. The second, which is adopted here, is to devise simple approximate procedures. Such procedures should promote a better understanding of the problem, and provide tables or charts of results as functions of as few parameters as practicable. The analysis is undertaken in references 1 and 2. The results obtained from that analysis are summarized in this report which is intended to be a reference for persons interested in using the results, but who are not concerned with the mathematical derivations. | |
| language | English | |
| title | NASA-TN-D-402 | num |
| title | Analysis of frame-reinforced cylindrical shells. Part III - Applications | en |
| type | standard | |
| page | 137 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1960 | |
| contenttype | fulltext | |
| subject keywords | ANALYSIS | |
| subject keywords | CYLINDRICAL | |
| subject keywords | DATA | |
| subject keywords | DISPLACEMENT | |
| subject keywords | DISTRIBUTION | |
| subject keywords | FORCES | |
| subject keywords | LOADS | |
| subject keywords | MATHEMATICAL | |
| subject keywords | MODELS | |
| subject keywords | MOMENT | |
| subject keywords | NONUNIFORMITY | |
| subject keywords | RADIAL | |
| subject keywords | REINFORCED | |
| subject keywords | SHELLS | |
| subject keywords | STRESS | |
| subject keywords | TABLES |