| contributor author | J. D. Cyrus | |
| contributor author | P. F. Piscopo | |
| contributor author | R. T. Lazarick | |
| date accessioned | 2017-05-08T23:13:16Z | |
| date available | 2017-05-08T23:13:16Z | |
| date copyright | April, 1982 | |
| date issued | 1982 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26772#314_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/95792 | |
| description abstract | Engine-aircraft mission studies have been conducted by the Navy to establish changes in the weight and performance of supersonic VSTOL aircraft resulting from changes in the main cruise engine configuration, cycle characteristics, and complexity. The effects of engine component efficiency variations were quantified by a sensitivity analysis which identified performance changes on four different missions for a single engine aircraft. Studies of a twin engine aircraft with four different propulsion system configurations established the impact of changes in various cycle parameters on aircraft takeoff gross weight for the same three missions and identified thermodynamic and physical constraints for the cycles. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Establishing Cruise-Engine Cycle Payoffs for a Supersonic VSTOL Aircraft | |
| type | Journal Paper | |
| journal volume | 104 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3227281 | |
| journal fristpage | 314 | |
| journal lastpage | 319 | |
| identifier eissn | 0742-4795 | |
| keywords | Aircraft | |
| keywords | Cycles | |
| keywords | Engines | |
| keywords | Weight (Mass) | |
| keywords | Propulsion systems | |
| keywords | Navy AND Sensitivity analysis | |
| tree | Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002 | |
| contenttype | Fulltext | |
