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Knowledge Management System of Institue of Mechanics, CAS
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刘文 [3]
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Indexed By:SCI
Source Publication:AIAA Journal
Community:高温气体动力学国家重点实验室
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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
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Submit date:2021/08/30
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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View/Download:567/135
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Submit date:2020/05/07
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
Starting Process in a Large-Scale Shock Tunnel
期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2017/09/19
Concept of non-ablative thermal protection system for hypersonic vehicles
期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:1418/509
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Submit date:2013/04/07
Flow Fields
Flow Visualization
Hypersonic Aerodynamics
Hypersonic Vehicles
Mach Number
Shock Waves
Thermal Insulating Materials
Engineering Applications
Experimental Datum
Hypersonic Wind Tunnels
Numerical Results
Stagnation Points
Thermal Protection
Thermal Protection System
Working Pressures