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Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194
Authors:
Duan JY(段俊亦)
;
Tong FL(童福林)
;
Li XL(李新亮)
;
Liu HW(刘洪伟)
Adobe PDF(6039Kb)
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Submit date:2023/11/13
Compressible flow
Boundary layers
Direct numerical simulation
Shock waves
Skin friction
Turbulent flow
Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
Authors:
Peng J(彭俊)
;
Li S(李帅)
;
Yang F(杨帆)
;
Lin MY(林明月)
;
Han GL(韩桂来)
;
Hu ZM(胡宗民)
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Submit date:2023/04/20
Shock interactions
Transitional configuration
Aerodynamic heating
Shear layer
Mach interaction
A new dynamic subgrid-scale model using artificial neural network for compressible flow
期刊论文
THEORETICAL AND APPLIED MECHANICS LETTERS, 2022, 卷号: 12, 期号: 4
Authors:
Qi H(齐涵)
;
Li XL(李新亮)
;
Luo, Ning
;
Yu ZP(于长平)
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Submit date:2024/01/15
Subgrid-scale kinetic energy
Eddy-viscosity model
Compressible flow
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)
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Submit date:2021/11/01
CO2-based mixture
flammability
laminar flame speed
flammable critical mixing ratio
transcritical power cycle
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)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
On theory and methods for advanced detonation-driven hypervelocity shock tunnels
期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:
Jiang ZL(姜宗林)
;
Li JP(李进平)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Yu HR(俞鸿儒)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
Shock relations in gases of heterogeneous thermodynamic properties
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:
Hu ZM(胡宗民)
;
Zhou K(周凯)
;
Peng J(彭俊)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
;
Li, JP (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:2017/10/25
Shock Wave
Imperfect Gas
Heterogeneous
Theoretical Solution
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Hu ZM(胡宗民)
;
Li XD
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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Submit date:2016/12/08
3d Asymmetrical Shock/shock Interaction
Spatial-dimension Reduction
Mach Reflection
Flow Field
Theoretical Analysis
Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 7, 页码: 1120-1129
Authors:
Li, XD
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
;
Hu, ZM (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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View/Download:301/99
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Submit date:2016/09/14
Hypersonic Flow
Aerodynamic Heating
Thermal Protection System
Forward-facing Cavity
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Chen, LH (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:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm