| 舰载直升机风限图及其试飞 |
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| 引用本文： | 赵维义,刘航,傅百先.舰载直升机风限图及其试飞[J].飞行力学,2002,20(4):48-50,60. |
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| 作者姓名： | 赵维义 刘航 傅百先 |
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| 作者单位： | 海军航空工程学院,青岛分院,山东,青岛,266041 |
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| 摘 要： | 首先介绍了确定理论风限图的方法，然后阐述－舰动态配合试验的原则和实施方法，以及试验的技术要求和所要达到的目的，并详细分析了试飞过程中各个阶段的内容和要求。最后，给出了一些进一步试飞的意见和建议。
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| 关 键 词： | 舰载直升机 风限图 飞行试验 |
| 文章编号： | 1002-0853(2002)04-0048-03 |
Safe Operating Envelopes of Onboard Helicopter and Its Flight Test |
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| ZHAO Wei-yi,LIU Hang,FU Bai-xian.Safe Operating Envelopes of Onboard Helicopter and Its Flight Test[J].Flight Dynamics,2002,20(4):48-50,60. |
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| Authors: | ZHAO Wei-yi LIU Hang FU Bai-xian |
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| Abstract: | Firstly this paper introduces the methods of determining a theoretical launch and recovery wind-limitation envelope. And then it discusses the principles and executing methods of helicopter/ship dynamic interface testing, technical requirements and its aim. Besides, the contents and requirements at every phase of the flight test are analyzed. Lastly, some opinions and proposals for further flight test in the safe operating envelopes are presented. |
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| Keywords: | helicopter safe operating envelope flight test |
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