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| 海豚型直升机转弯机动飞行特性研究 | |
| 引用本文： | 许心钰 王威. 海豚型直升机转弯机动飞行特性研究[J]. 南京航空航天大学学报, 1994, 26(1): 121-126 |
| 作者姓名： | 许心钰 王威 |
| 作者单位： | 南京航空航天大学飞行器系 |
| 摘 要： | 本文以能量法研究直升机转弯机动飞行特性，这是评价一架直升机机动性能的基本要素之一。文中以海豚型直升机（直九）为算例，给出能量图和机动图，并利用能量法原理分析了直九机的自动转弯、下降转弯、减速转弯机动飞行特性，计算了各参数对这些转弯性能的影响。 |
| 关 键 词： | 直升机；飞行力学，机动飞行；能量法，机动飞行特性 |
Study on Z-9 Helicopter Turning Maneuver Characteristics by Energy Method |
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| Xu Xinyu,Wang Wei. Study on Z-9 Helicopter Turning Maneuver Characteristics by Energy Method[J]. Journal of Nanjing University of Aeronautics & Astronautics, 1994, 26(1): 121-126 | |
| Authors: | Xu Xinyu Wang Wei |
| Abstract: | The turning maneuver characteristics are one of the essential factors for evaluating the helicopter maneuver characteristics. The energy and maneuver diagram are made in this paper. Using the energy method the maneuver flight characteristics of the deceleration turning, auto-turning and desending turning are analyzed and the influence of the parameters on the turning characteristics are calculated. |
| Keywords: | helicopters flight mechanics maneuver flight energy method maneuverflight characteristics |
| 本文献已被 CNKI 维普 等数据库收录！ | |