| contributor author | K. R. Hedges | |
| contributor author | P. G. Hill | |
| date accessioned | 2017-05-09T01:38:19Z | |
| date available | 2017-05-09T01:38:19Z | |
| date copyright | September, 1974 | |
| date issued | 1974 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26860#282_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/164880 | |
| description abstract | An experimental study has been made of compressible jet mixing in an axisymmetric ejector of converging-diverging geometry. The mass flow ratio was in the range 1.3 to 2.6 and the nozzle exit Mach number was 1.82. Ejector performance characteristics were obtained as well as measurements of pressure and velocity distribution over a range of mass flow rates. The experimental results were used to test the reliability of the analytical model of the flow described in Part I of the paper. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Compressible Flow Ejectors: Part II—Flow Field Measurements and Analysis | |
| type | Journal Paper | |
| journal volume | 96 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3447153 | |
| journal fristpage | 282 | |
| journal lastpage | 288 | |
| identifier eissn | 1528-901X | |
| keywords | Flow (Dynamics) | |
| keywords | Measurement | |
| keywords | Ejectors | |
| keywords | Compressible flow | |
| keywords | Geometry | |
| keywords | Performance characterization | |
| keywords | Nozzles | |
| keywords | Reliability | |
| keywords | Mach number AND Pressure | |
| tree | Journal of Fluids Engineering:;1974:;volume( 096 ):;issue: 003 | |
| contenttype | Fulltext | |
