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NASA-TN-D-5054
Experimental pressure distributions on a 120 degrees cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0 degrees to 20 degrees
Year: 1969
Abstract: Experimental pressure distributions on 120 deg cone at Mach 2.96 to 4.63 and angles of attack from 0 deg to 20 deg
Subject: BLUNT
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:50:45Z | |
| date available | 2017-09-04T15:50:45Z | |
| date copyright | 01/01/1969 | |
| date issued | 1969 | |
| identifier other | QHYKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/53871 | |
| description abstract | Experimental pressure distributions on 120 deg cone at Mach 2.96 to 4.63 and angles of attack from 0 deg to 20 deg | |
| language | English | |
| title | NASA-TN-D-5054 | num |
| title | Experimental pressure distributions on a 120 degrees cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0 degrees to 20 degrees | en |
| type | standard | |
| page | 79 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1969 | |
| contenttype | fulltext | |
| subject keywords | BLUNT | |
| subject keywords | BODIES | |
| subject keywords | CONES | |
| subject keywords | DISTRIBUTION | |
| subject keywords | FLOW | |
| subject keywords | FRUSTUMS | |
| subject keywords | MACH | |
| subject keywords | NUMBER | |
| subject keywords | PRESSURE | |
| subject keywords | PROFILES | |
| subject keywords | SHOCK | |
| subject keywords | SLENDER | |
| subject keywords | SUPERSONIC | |
| subject keywords | WAVE |