| 悬挂对飞行器静稳定性影响的分析论证 |
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| 引用本文： | 李怡勇,沈怀荣. 悬挂对飞行器静稳定性影响的分析论证[J]. 装备指挥技术学院学报, 2004, 15(6): 56-59. DOI: 10.3783/j.issn.1673-0127.2004.06.015 |
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| 作者姓名： | 李怡勇 沈怀荣 |
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| 作者单位： | 1. 装备指挥技术学院,研究生部,北京,101416
2. 装备指挥技术学院,试验工程系,北京,101416 |
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| 摘 要： | 静稳定性与飞行器设计及飞行品质有密切关系。用建模的思想,把复杂的实际系统合理简化,在理论上论证了悬挂稳定的可行性,研究了稳定效果与影响因素之间的关系,并提出了设计改进方案,作为进一步实验论证的理论依据。
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| 关 键 词： | 悬挂 稳定性 静稳定性 稳定能力 |
| 文章编号： | 1673-0127(2004)06-0056-04 |
| 修稿时间： | 2004-04-13 |
Analysis and Study to Hanging Effect to Aircraft Static Stability |
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| LI Yi-yong,SHEN Huai-rong. Analysis and Study to Hanging Effect to Aircraft Static Stability[J]. Journal of the Academy of Equipment Command & Technology, 2004, 15(6): 56-59. DOI: 10.3783/j.issn.1673-0127.2004.06.015 |
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| Authors: | LI Yi-yong SHEN Huai-rong |
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| Affiliation: | LI Yi-yong~1,SHEN Huai-rong~2 |
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| Abstract: | Static stability is closely concerned with aircraft's design and flight quality. Based on the idea of modeling, the paper reasonably predigests a complicated actual system, demonstrates the feasibility of hanging method in theory, studies connection between stability and influencing factors, and brings forward an improved method of design that can be regarded as academic basis for further experiments. |
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| Keywords: | hanging stability static stability stabilizing ability |
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