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亚轨道飞行器再入攻角设计的法向过载动平衡方法
李文皓; 肖歆昕; 张珩
Source Publication第三届高超声速科技学术会议.江苏·无锡.2010年10月26-28日
2010-10-26
Conference Name第三届高超声速科技学术会议
Conference Place江苏·无锡
Abstract对亚轨道飞行器再入飞行轨迹及热流、动压及过载等指标的演化过程展开研究,总结了亚轨道飞行器再入过程中法向过载较高的特点,分析了其形成原因。针对该问题,提出了一种基于法向过载动态平衡的亚轨道飞行器再入攻角设计方法,设计了其实现算法。通过对某型亚轨道飞行器再入攻角设计的仿真验证,其结果表明,基于法向过载动态平衡的攻角设计方法可有效降低再入法向过载峰值。文章的最后,对该方法的应用前景进行了展望。
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Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/44285
Collection先进制造工艺力学实验室
Corresponding Author李文皓
Recommended Citation
GB/T 7714
李文皓,肖歆昕,张珩. 亚轨道飞行器再入攻角设计的法向过载动平衡方法[C]第三届高超声速科技学术会议.江苏·无锡.2010年10月26-28日,2010.
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