| 一种复合升力飞机模型的设计与飞行验证 |
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| 引用本文： | 曹飞,詹浩.一种复合升力飞机模型的设计与飞行验证[J].飞行力学,2012,30(1):9-12. |
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| 作者姓名： | 曹飞 詹浩 |
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| 作者单位： | 西北工业大学航空学院,陕西西安,710072 |
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| 摘 要： | 针对一种复合升力飞机,建立了相应的研究模型,通过试验、CFD计算和工程估算的方法,研究了直升机和固定翼状态下的飞机性能特性,并通过制作一架模型验证机,验证了该种飞机飞行原理的可行性,并提出了一些意见。
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| 关 键 词： | 复合升力飞机 性能特性 飞行原理 |
Research on conceptual layout design and flight test for a multimode aircraft |
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| CAO Fei
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ZHAN Hao.Research on conceptual layout design and flight test for a multimode aircraft[J].Flight Dynamics,2012,30(1):9-12. |
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| Authors: | CAO Fei ZHAN Hao |
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| Institution: | (College of Aeronautics,NWPU,Xi’an 710072,China) |
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| Abstract: | In this paper,a multimode aircraft research model is built.The rotor mode and fix wing mode’s performance characters that have been researched by the experiment,CFD and the project evaluation methods.According to the aircraft flight test verification,the way of flight of the multimode aircraft is feasible,and provides some suggestions for improving its performance. |
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| Keywords: | multimode aircraft performance characteristics flight principle |
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