| 某型增压航空活塞发动机仿真研究 |
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| 引用本文： | 林海英,龙向阳.某型增压航空活塞发动机仿真研究[J].航空动力学报,2009,24(6):1332-1338. |
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| 作者姓名： | 林海英 龙向阳 |
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| 作者单位： | 1. 北京航空航天大学,无人驾驶飞行器研究所,北京,100191
2. 北京航空航天大学,能源与动力工程学院,北京,100191 |
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| 基金项目： | 航空科学基金(2008ZB51011) |
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| 摘 要： | 介绍了某型航空活塞发动机仿真模型的建立方法,建立了带有一级增压器的某型航空活塞发动机仿真模型,并进行了该发动机的地面特性的仿真计算,计算结果与试验结果符合得很好.在此基础上进行了该发动机高空特性的仿真计算,仿真结果与飞行试验数据较好地吻合,能够满足工程使用要求.
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| 关 键 词： | 活塞发动机 无人机 增压器 仿真模型 |
| 收稿时间： | 2008/4/25 0:00:00 |
| 修稿时间： | 2008/12/22 0:00:00 |
Simulation study of an aero-piston engine with single stage turbocharger |
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| LIN Hai-ying and LONG Xiang-yang.Simulation study of an aero-piston engine with single stage turbocharger[J].Journal of Aerospace Power,2009,24(6):1332-1338. |
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| Authors: | LIN Hai-ying and LONG Xiang-yang |
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| Institution: | 1.Unmanned Aircraft Institute;Beijing University of Aeronautics and Astronautics;Beijing 100191;China;2.School of Jet Propulsion;China |
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| Abstract: | The method was introduced for setting up simulation model of an aero-piston engine.The simulation model of an engine with single-stage turbocharger was set up,and the ground performance's simulation computation was finished.The simulation results were coincident with the test data.On the basis of the former works,the high altitude performance simulation was conducted,and the results were consistent with the fly test data. |
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| Keywords: | piston engine unmanned air vehicle turbocharger simulation model |
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