| 军用飞机设计方案易损性评估 |
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| 引用本文： | 崔荣洪,何宇廷.军用飞机设计方案易损性评估[J].飞机设计,2007,27(3):56-58. |
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| 作者姓名： | 崔荣洪 何宇廷 |
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| 作者单位： | 空军工程大学,工程学院,陕西,西安,710038 |
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| 摘 要： | 在系统分析军用飞机设计方案易损性评估特点的基础上,给出了适用的易损性评估方法——加权综合评价指数法,以及评估准则和加权权重系数的确定方法。最后,给出了应用的实例。
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| 关 键 词： | 军用飞机设计方案 易损性评估 加权综合指数 |
| 文章编号： | 1673-4599（2007）03-0056-03 |
| 收稿时间： | 2006-09-25 |
| 修稿时间： | 2006-09-252007-04-15 |
Vulnerability Assessment of Military Aircraft Design |
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| CUI Rong-hong,HE Yu-ting.Vulnerability Assessment of Military Aircraft Design[J].Aircraft Design,2007,27(3):56-58. |
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| Authors: | CUI Rong-hong HE Yu-ting |
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| Abstract: | Based on the analyses of the characteristics of vulnerability assessment of military aircraft design,a suitable assessment method(weighting composite index assessment method)is presented.An approach to evaluating weighting coefficients is proposed.And finally,an application example is given to demonstrate the assessment method. |
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| Keywords: | military aircraft design vulnerability assessment weighting composite index |
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