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NASA-TN-D-2042
Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at mach numbers from 1.57 to 2.86
Year: 1963
Abstract: Afterbody geometry and sting diameter effect on aerodynamics of slender bodies at supersonic speed
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:01:59Z | |
| date available | 2017-09-04T17:01:59Z | |
| date copyright | 01/01/1963 | |
| date issued | 1963 | |
| identifier other | XSTKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/125441 | |
| description abstract | Afterbody geometry and sting diameter effect on aerodynamics of slender bodies at supersonic speed | |
| language | English | |
| title | NASA-TN-D-2042 | num |
| title | Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at mach numbers from 1.57 to 2.86 | en |
| type | standard | |
| page | 32 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1963 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AERODYNAMICS | |
| subject keywords | AFTERBODIES | |
| subject keywords | AFTERBODY | |
| subject keywords | BOATS | |
| subject keywords | BODIES | |
| subject keywords | BODY | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | MACH | |
| subject keywords | MOUNTING | |
| subject keywords | NUMBER | |
| subject keywords | SLENDER | |
| subject keywords | SPEED | |
| subject keywords | SUPERSONIC |