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NASA-TM-X-1785
Jet effects on boattail pressure drag of isolated ejector nozzles at Mach numbers from 0.60 to 1.47
Year: 1969
Abstract: Jet effects on boattail pressure drag of isolated ejector nozzles at Mach 0.60 to 1.47
Subject: AIR
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:27:41Z | |
| date available | 2017-09-04T16:27:41Z | |
| date copyright | 01/01/1969 | |
| date issued | 1969 | |
| identifier other | UDNKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/90784 | |
| description abstract | Jet effects on boattail pressure drag of isolated ejector nozzles at Mach 0.60 to 1.47 | |
| language | English | |
| title | NASA-TM-X-1785 | num |
| title | Jet effects on boattail pressure drag of isolated ejector nozzles at Mach numbers from 0.60 to 1.47 | en |
| type | standard | |
| page | 91 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1969 | |
| contenttype | fulltext | |
| subject keywords | AIR | |
| subject keywords | BOATTAILS | |
| subject keywords | BOUNDARIES | |
| subject keywords | BREATHING | |
| subject keywords | DRAG | |
| subject keywords | EJECTORS | |
| subject keywords | ENGINES | |
| subject keywords | EXPANSION | |
| subject keywords | FLOW | |
| subject keywords | GAS | |
| subject keywords | JET | |
| subject keywords | NOZZLE | |
| subject keywords | PRESSURE | |
| subject keywords | SPEED | |
| subject keywords | SUBSONIC |