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NASA-TM-X-311
A wind-tunnel investigation of the aerodynamic characteristics of bodies of revolution at mach numbers of 2.37, 2.98, and 3.90 at angles of attack to 90 deg
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:23:12Z | |
| date available | 2017-09-04T18:23:12Z | |
| date copyright | 01/01/1960 | |
| date issued | 1960 | |
| identifier other | IDNKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/205643 | |
| description abstract | High angle aerodynamic characteristics produced by nose cone of revolution in wind tunnel at supersonic speed | |
| language | English | |
| title | NASA-TM-X-311 | num |
| title | A wind-tunnel investigation of the aerodynamic characteristics of bodies of revolution at mach numbers of 2.37, 2.98, and 3.90 at angles of attack to 90 deg | en |
| type | standard | |
| page | 35 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1960 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | BODIES | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | CONE | |
| subject keywords | CONES | |
| subject keywords | MACH | |
| subject keywords | NOSE | |
| subject keywords | NUMBER | |
| subject keywords | REVOLUTION | |
| subject keywords | SPEED | |
| subject keywords | SUPERSONIC | |
| subject keywords | TUNNEL | |
| subject keywords | TUNNELS | |
| subject keywords | WIND |
