درباره ما
NASA-TM-X-1517
Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies
Year: 1968
Abstract: Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies of supersonic engine nacelles
Subject: AERODYNAMIC
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:05:59Z | |
| date available | 2017-09-04T15:05:59Z | |
| date copyright | 01/01/1968 | |
| date issued | 1968 | |
| identifier other | LDNKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/3477 | |
| description abstract | Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies of supersonic engine nacelles | |
| language | English | |
| title | NASA-TM-X-1517 | num |
| title | Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies | en |
| type | standard | |
| page | 35 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1968 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AFTERBODIES | |
| subject keywords | BOATTAILS | |
| subject keywords | BODIES | |
| subject keywords | COEFFICIENTS | |
| subject keywords | CONFIGURATIONS | |
| subject keywords | CONICAL | |
| subject keywords | DISTRIBUTION | |
| subject keywords | DRAG | |
| subject keywords | FLOW | |
| subject keywords | GEOMETRY | |
| subject keywords | MODELS | |
| subject keywords | NACELLES | |
| subject keywords | NOZZLE | |
| subject keywords | PRESSURE | |
| subject keywords | SUPERSONIC | |
| subject keywords | TUNNEL | |
| subject keywords | WIND |