| contributor author | J. A. C. Kentfield | |
| contributor author | M. Rehman | |
| contributor author | E. S. Marzouk | |
| date accessioned | 2017-05-08T23:02:48Z | |
| date available | 2017-05-08T23:02:48Z | |
| date copyright | April, 1977 | |
| date issued | 1977 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26732#153_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/89815 | |
| description abstract | The performance is presented, and a description is given, of a simple pressure-gain combustor, without moving parts, which has been shown, during laboratory trials, to produce a stagnation pressure-gain across the combustor in excess of 5 percent at a combustor stagnation temperature of 3:1. It is also shown that the concept of the device appears to lend itself to development in such a way that it should be possible to incorporate successfully combustors based on the prototype in many gas turbines. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Simple Pressure-Gain Combustor for Gas Turbines | |
| type | Journal Paper | |
| journal volume | 99 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3446261 | |
| journal fristpage | 153 | |
| journal lastpage | 158 | |
| identifier eissn | 0742-4795 | |
| keywords | Pressure | |
| keywords | Combustion chambers | |
| keywords | Gas turbines | |
| keywords | Engineering prototypes AND Temperature | |
| tree | Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 002 | |
| contenttype | Fulltext | |
