| contributor author | R. L. Binsley | |
| contributor author | J. L. Boynton | |
| date accessioned | 2017-05-08T23:04:43Z | |
| date available | 2017-05-08T23:04:43Z | |
| date copyright | April, 1978 | |
| date issued | 1978 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26740#197_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/90988 | |
| description abstract | The detailed aerodynamic design and test verification of a 6000-hp (4474-kW) turbine with a supersonic first stage for an airborne application is described. The 12.3-in. (312.4-mm) pitch diameter turbine is driven by products of hydrazine decomposition at 700 psia (4.826 MPa) and 2110 R (1172 K) with an overall pressure ratio of 41.2. The design of the supersonic nozzles and rotor incorporated improved concepts compared to previously reported designs. Test results show that the predicted performance was verified. The supersonic design concepts described are applicable to other high-pressure ratio designs where maximum efficiency is required. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Aerodynamic Design and Verification of a Two-Stage Turbine With a Supersonic First Stage | |
| type | Journal Paper | |
| journal volume | 100 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3446333 | |
| journal fristpage | 197 | |
| journal lastpage | 202 | |
| identifier eissn | 0742-4795 | |
| keywords | Design | |
| keywords | Turbines | |
| keywords | Nozzles | |
| keywords | Rotors | |
| keywords | Pressure AND High pressure (Physics) | |
| tree | Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 002 | |
| contenttype | Fulltext | |
