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NASA-TM-X-1658
Aerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of attack to 180 deg
Year: 1968
Abstract: Aerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of attack to 180 deg
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:31:22Z | |
| date available | 2017-09-04T15:31:22Z | |
| date copyright | 01/01/1968 | |
| date issued | 1968 | |
| identifier other | ODNKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/32901 | |
| description abstract | Aerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of attack to 180 deg | |
| language | English | |
| title | NASA-TM-X-1658 | num |
| title | Aerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of attack to 180 deg | en |
| type | standard | |
| page | 41 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1968 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | BODIES | |
| subject keywords | CENTER | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | DESCENT | |
| subject keywords | FINENESS | |
| subject keywords | FOREBODIES | |
| subject keywords | GRAVITY | |
| subject keywords | LONGITUDINAL | |
| subject keywords | NOSES | |
| subject keywords | NUMBER | |
| subject keywords | PARACHUTE | |
| subject keywords | PAYLOADS | |
| subject keywords | RATIO | |
| subject keywords | REVOLUTION | |
| subject keywords | REYNOLDS | |
| subject keywords | SPEED | |
| subject keywords | STABILITY | |
| subject keywords | SUPERSONIC | |
| subject keywords | TUNNELS | |
| subject keywords | WIND |