| contributor author | J. C. Dutton | |
| contributor author | B. F. Carroll | |
| date accessioned | 2017-05-08T23:22:41Z | |
| date available | 2017-05-08T23:22:41Z | |
| date copyright | December, 1986 | |
| date issued | 1986 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27023#414_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101271 | |
| description abstract | A technique based on a one-dimensional constant area flow model has been developed for solving a large class of supersonic ejector optimization problems. In particular, the method determines the primary nozzle Mach number and ejector area ratio which optimizes either the entrainment ratio, compression ratio, or stagnation pressure ratio given values for the other two variables and the primary and secondary gas properties and stagnation temperatures. Design curves for the common case of diatomic primary and secondary gases of equal molecular weight and stagnation temperature are also presented and discussed. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Optimal Supersonic Ejector Designs | |
| type | Journal Paper | |
| journal volume | 108 | |
| journal issue | 4 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3242597 | |
| journal fristpage | 414 | |
| journal lastpage | 420 | |
| identifier eissn | 1528-901X | |
| keywords | Ejectors | |
| keywords | Temperature | |
| keywords | Gases | |
| keywords | Design | |
| keywords | Pressure | |
| keywords | Flow (Dynamics) | |
| keywords | Mach number | |
| keywords | Nozzles | |
| keywords | Optimization | |
| keywords | Compression AND Molecular weight | |
| tree | Journal of Fluids Engineering:;1986:;volume( 108 ):;issue: 004 | |
| contenttype | Fulltext | |