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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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余西龙 [1]
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Community:高温气体动力学国家重点实验室
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空天进入飞行器新概念气动布局研究
学位论文
博士论文,北京: 中国科学院大学, 2021
Authors:
徐应洲
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View/Download:646/26
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Submit date:2021/06/04
高压捕获翼
动导数
飞行仿真
稳定性
基于扭摆台架的动态推力测试方法研究
期刊论文
推进技术, 2017, 卷号: 38, 期号: 04, 页码: 925-931
Authors:
刘旭辉
;
杨飞虎
;
魏延明
;
陈君
;
汪旭东
;
毛威
;
李飞
;
余西龙
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View/Download:392/93
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Submit date:2017/12/22
微推力器
动态推力
扭摆台架
干涉式激光位移计
飞行器稳定性导数的参数辨识
会议论文
2016海峡两岸流体力学研讨会, 中国青海西宁, 2016-09-04
Authors:
聂雪媛
;
杨国伟
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View/Download:270/81
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Submit date:2017/09/27
配平攻角
稳定性导数
飞行器控制系统
动态稳定性
运动形态
飞行器设计
参数辨识
稳定性分析
风洞实验
飞行试验