درباره ما
NASA-TN-D-6435
Preliminary investigation of diffuser wall bleed to control combustor inlet airflow distribution
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:25:02Z | |
| date available | 2017-09-04T15:25:02Z | |
| date copyright | 01/01/1971 | |
| date issued | 1971 | |
| identifier other | NKBBFEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/25501 | |
| description abstract | Velocity profile control tests of diffuser wall bleed to control combustor inlet airflow distribution. | |
| language | English | |
| title | NASA-TN-D-6435 | num |
| title | Preliminary investigation of diffuser wall bleed to control combustor inlet airflow distribution | en |
| type | standard | |
| page | 19 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1971 | |
| contenttype | fulltext | |
| subject keywords | ANNULAR FLOW | |
| subject keywords | BOUNDARY LAYER CONTROL | |
| subject keywords | COMBUSTION CHAMBERS | |
| subject keywords | ENGINE INLETS | |
| subject keywords | GAS TURBINES | |
| subject keywords | INLET FLOW | |
| subject keywords | PRESSURE REDUCTION | |
| subject keywords | VELOCITY DISTRIBUTION |
