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NASA-LLIS-0652
Lessons Learned – Combination Methods for Deriving Structural Design Loads Considering Vibro-Acoustic, etc., Responses
Year: 2000
Abstract: Practice:
Design primary and secondary structural components to accommodate loads which include steadystate, transient dynamic, and vibro-acoustic contributions at liftoff.
Design primary and secondary structural components to accommodate loads which include steadystate, transient dynamic, and vibro-acoustic contributions at liftoff.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:25:56Z | |
| date available | 2017-09-04T18:25:56Z | |
| date copyright | 03/02/2000 | |
| date issued | 2000 | |
| identifier other | IKCEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/208110 | |
| description abstract | Practice: Design primary and secondary structural components to accommodate loads which include steadystate, transient dynamic, and vibro-acoustic contributions at liftoff. | |
| language | English | |
| title | NASA-LLIS-0652 | num |
| title | Lessons Learned – Combination Methods for Deriving Structural Design Loads Considering Vibro-Acoustic, etc., Responses | en |
| type | standard | |
| page | 6 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |