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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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Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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Submit date:2022/08/23
Aerodynamic Coefficients
Two Stage to Orbit
Aerodynamic Performance
Hypersonic Flight
Hypersonic Wind Tunnels
Solenoid Valves
Oblique Shock
Pneumatic Actuator
Hypersonic Flows
Computer Aided Engineering
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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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
Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula
期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 6, 页码: 1492-1502
Authors:
Liu TS
;
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
;
Liu, TS (reprint author), Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA.
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Submit date:2016/01/08
Evaluation of Lift Formulas Applied to Low-Reynolds-Number Unsteady Flows
期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 1, 页码: 161-175
Authors:
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
;
Liu TS
;
He, GW (reprint author), Chinese Acad Sci, State Key Lab Nonlinear Mech, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2015/03/17
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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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
Direct Numerical Simulation Of Hypersonic Boundary-Layer Transition Over A Blunt Cone
期刊论文
AIAA Journal, 2008, 页码: 2899-2913
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Lab Nonlinear Mech, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Hyperbolic Conservation-laws
Chemical kinetics and self-ignition in a model supersonic hydrogen-air combustor
期刊论文
AIAA Journal, 1999, 卷号: 37, 期号: 2, 页码: 208-214
Authors:
Sung CJ
;
Li JG(李建国)
;
Yu G(俞刚)
;
Sung, CJ (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
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Submit date:2007/06/15