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NASA-CR-413
Linear aerodynamic loads on cone-cylinders at Mach numbers from 0.7 to 2.0
Year: 1966
Abstract: Linear aerodynamic loads for cone-cylinder configurations in trisonic range
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:44:48Z | |
| date available | 2017-09-04T18:44:48Z | |
| date copyright | 01/01/1966 | |
| date issued | 1966 | |
| identifier other | KFNKAEAAAAAAAAAA.pdf | |
| identifier uri | https://lib.yabesh.ir/std/handle/yse/226185 | |
| description abstract | Linear aerodynamic loads for cone-cylinder configurations in trisonic range | |
| language | English | |
| title | NASA-CR-413 | num |
| title | Linear aerodynamic loads on cone-cylinders at Mach numbers from 0.7 to 2.0 | en |
| type | standard | |
| page | 88 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1966 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | CONE | |
| subject keywords | CONES | |
| subject keywords | CYLINDER | |
| subject keywords | CYLINDERS | |
| subject keywords | DISTRIBUTION | |
| subject keywords | FORCES | |
| subject keywords | LOAD | |
| subject keywords | LOADS | |
| subject keywords | SPEED | |
| subject keywords | SUBSONIC | |
| subject keywords | TRISONIC | |
| subject keywords | TUNNELS | |
| subject keywords | WIND |