| contributor author | M. R. Maltby | |
| date accessioned | 2017-05-08T23:24:45Z | |
| date available | 2017-05-08T23:24:45Z | |
| date copyright | April, 1987 | |
| date issued | 1987 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26644#127_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/102443 | |
| description abstract | The desirability of good acceleration behavior from helicopter gas turbine engines is discussed in the context of the increasing demand for helicopter maneuverability and safety. Features which result in improved engine handling qualities are discussed and reference is made to some analytical techniques which may be employed to assist in obtaining the best results. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Acceleration Performance of Helicopter Engines | |
| type | Journal Paper | |
| journal volume | 109 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3240014 | |
| journal fristpage | 127 | |
| journal lastpage | 131 | |
| identifier eissn | 0742-4795 | |
| keywords | Engines | |
| keywords | Gas turbines AND Safety | |
| tree | Journal of Engineering for Gas Turbines and Power:;1987:;volume( 109 ):;issue: 002 | |
| contenttype | Fulltext | |
