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NASA-TN-D-5392
Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2.49 to 4.63 and angles of attack from 0 degrees to 15 degrees
Year: 1969
Abstract: Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack from 0 to 15 degrees
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:25:27Z | |
| date available | 2017-09-04T18:25:27Z | |
| date copyright | 01/01/1969 | |
| date issued | 1969 | |
| identifier other | IIYKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/207651 | |
| description abstract | Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack from 0 to 15 degrees | |
| language | English | |
| title | NASA-TN-D-5392 | num |
| title | Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2.49 to 4.63 and angles of attack from 0 degrees to 15 degrees | en |
| type | standard | |
| page | 88 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1969 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | BALLISTICS | |
| subject keywords | BLUNT | |
| subject keywords | BODIES | |
| subject keywords | CYLINDRICAL | |
| subject keywords | DATA | |
| subject keywords | DISTRIBUTION | |
| subject keywords | HEATING | |
| subject keywords | MODELS | |
| subject keywords | PRESSURE | |
| subject keywords | REENTRY | |
| subject keywords | REVOLUTION | |
| subject keywords | SPEED | |
| subject keywords | SUPERSONIC | |
| subject keywords | TABLES | |
| subject keywords | TUNNEL | |
| subject keywords | VEHICLES | |
| subject keywords | WIND |