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Indexed By:CSCD
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Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences
期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:
Lin MY(林明月)
;
Yang F(杨帆)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
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View/Download:5/0
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Submit date:2024/05/27
Shock waves
Shock-shock interaction
Theoretical analysis
Hysteresis
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:
Yuan CK(苑朝凯)
;
Meng FZ(孟凡钊)
;
Liu, Xu
;
Liu YF(刘云峰)
;
Lian H(连欢)
;
Liu, Yingzheng
;
Peng, Di
Adobe PDF(3477Kb)
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Submit date:2023/07/17
Temperature-sensitive paint
Heat flux
Conjugate gradient method
Air-breathing hypersonic vehicle
Inverse heat conduction problem
Oblique detonation wave triggered by a double wedge in hypersonic flow
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184
Authors:
Teng, Honghui
;
Zhang, Yuhang
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(1747Kb)
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Submit date:2022/07/18
Double wedge
Hypersonic flow
Initiation structures
Oblique detonation
Shock interactions
Reconstructing shock front of unstable detonations based on multi-layer perceptron
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:
Zhou, Lin
;
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(6382Kb)
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Submit date:2021/11/01
Cellular detonation
Lead shock evolution
Multi-layer perceptron
Numerical simulations
Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2
期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12
Authors:
Shi Weixiu
;
Pan LS(潘利生)
;
Jin Suyi
;
Dong YH(董跃华)
;
Li T(李腾)
;
Zhao J(赵京)
;
Wei XL(魏小林)
Adobe PDF(2198Kb)
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Submit date:2021/11/01
CO2-based mixture
flammability
laminar flame speed
flammable critical mixing ratio
transcritical power cycle
Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:
Tong FL(童福林)
;
Sun D(孙栋)
;
Li XL(李新亮)
Adobe PDF(4402Kb)
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View/Download:213/50
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Submit date:2021/06/07
Direct numerical simulation
Low-frequency unsteadiness
Shock waves
Turbulent boundary layer
Wavy-wall
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
Authors:
Peng, Di
;
Liu, Xu
;
Jiao, Lingrui
;
Li, Ziyan
;
Wen, Xin
;
Yuan CK(苑朝凯)
;
Han GL(韩桂来)
;
Liu YF(刘云峰)
;
Liu, Yingzheng
;
Jiang ZL(姜宗林)
Adobe PDF(3477Kb)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:
Yuan CK(苑朝凯)
;
Jiang ZL(姜宗林)
Adobe PDF(3790Kb)
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View/Download:403/65
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
Adobe PDF(1129Kb)
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train