| contributor author | Y. Tsujikawa | |
| contributor author | M. Nagaoka | |
| date accessioned | 2017-05-08T23:35:35Z | |
| date available | 2017-05-08T23:35:35Z | |
| date copyright | January, 1991 | |
| date issued | 1991 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26683#100_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/108575 | |
| description abstract | This paper is devoted to the analyses and optimization of simple and sophisticated cycles, particularly for various gas turbine engines and aero-engines (including the scramjet engine) to achieve maximum performance. The optimization of such criteria as thermal efficiency, specific output, and total performance for gas turbine engines, and overall efficiency, nondimensional thrust, and specific impulse for aero-engines has been performed by the optimization procedure with the multiplier method. Comparison of results with analytical solutions establishes the validity of the optimization procedure. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Determination of Cycle Configuration of Gas Turbines and Aircraft Engines by an Optimization Procedure | |
| type | Journal Paper | |
| journal volume | 113 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2906515 | |
| journal fristpage | 100 | |
| journal lastpage | 105 | |
| identifier eissn | 0742-4795 | |
| keywords | Gas turbines | |
| keywords | Optimization | |
| keywords | Cycles | |
| keywords | Aircraft engines | |
| keywords | Thrust | |
| keywords | Impulse (Physics) AND Scramjets | |
| tree | Journal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 001 | |
| contenttype | Fulltext | |
