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中国科学院力学研究所机构知识库
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王发民 [33]
张陈安 [13]
韩汉桥 [8]
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高超声速钝前缘乘波构型优化设计研究
期刊论文
力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1414-1428
Authors:
郭帅旗
;
刘文
;
张陈安
;
王发民
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Submit date:2022/08/11
高超声速
乘波体
前缘钝化
Parametric Study on Lateral–Directional Stability of Hypersonic Waverider
期刊论文
AIAA Journal, 2021, 卷号: 59, 期号: 8, 页码: 3025-3042
Authors:
刘文
;
张陈安
;
Wang Xiao-Peng
;
Li Jin-Jie
;
王发民
Adobe PDF(7528Kb)
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Submit date:2021/08/30
Design of a new supersonic biplane
期刊论文
Acta Astronautica, 2020, 卷号: 175, 期号: 10, 页码: 216-233
Authors:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW
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Submit date:2020/06/08
Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines
期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5
Authors:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW
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Submit date:2020/08/26
Hypersonic inlet
lateral spillage
waverider design method
streamline tracing technology
mass-flow ratio
Design and Optimization Method for Hypersonic Quasi-Waverider
期刊论文
AIAA Journal, 2020, 卷号: 58, 期号: 5, 页码: 2132-2146
Authors:
Liu W(刘文)
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Ye ZY
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Submit date:2020/05/07
Modification of hypersonic waveriders by vorticity-based boundary layer displacement thickness determination method
期刊论文
Aerospace Science and Technology, 2018, 卷号: 75, 页码: 200-214
Authors:
Liu W(刘文)
;
Zhang CA(张陈安)
;
Wang FM(王发民)
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Submit date:2018/06/16
Local Piston Theory with Viscous Correction and Its Application
期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
Authors:
Liu W(刘文)
;
Zhang CA(张陈安)
;
Han HQ
;
Wang FM(王发民)
;
Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2017/03/28
Hypersonic
Unsteady Aerodynamics
Piston Theory
Aeroelasticity
一种高空高超声速非定常气动力近似模型
期刊论文
力学学报, 2013, 卷号: 45, 期号: 5, 页码: 690-698
Authors:
韩汉桥
;
张陈安
;
王发民
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Submit date:2013/11/18
高超声速
黏性干扰
非定常气动力
当地流活塞理论
黏性修正
钝化前缘乘波布局及其一体化构型气动特性
期刊论文
航空动力学报, 2013, 卷号: 28, 期号: 2, 页码: 379-384
Authors:
陈雪冬
;
王发民
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Submit date:2013/03/07
钝化前缘
高超声速
乘波布局
一体化构型
气动特性
Aerodynamic and Aerothermal Performance of Power-law Shaped Leading Edge of Hypersonic Waveriders
期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 207-217
Authors:
Wang FM(王发民)
;
Han HQ(韩汉桥)
;
Lei MF(雷麦芳)
;
Zhang J(张杰)
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Submit date:2015/09/24
Aerothermal Protection
Power-law Leading Edge
Aerodynamic Performance