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Source Publication:AIAA JOURNAL
Document Type:期刊论文
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Assessment of Regularized Ensemble Kalman Method for Inversion of Turbulence Quantity Fields
期刊论文
AIAA JOURNAL, 2022, 卷号: 60, 期号: 1, 页码: 3-13
Authors:
Zhang XL(张鑫磊)
;
Xiao, Heng
;
He GW(何国威)
Adobe PDF(1913Kb)
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Submit date:2022/01/24
Acoustic Inversion for Uncertainty Reduction in Reynolds-Averaged Navier-Stokes-Based Jet Noise Prediction
期刊论文
AIAA JOURNAL, 2022, 卷号: 60, 期号: 7, 页码: 2407-2422
Authors:
Zhang XL(张鑫磊)
;
Xiao, Heng
;
Wu T(吴霆)
;
He GW(何国威)
Adobe PDF(9316Kb)
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Submit date:2022/03/05
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing
期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:
Lin MY(林明月)
;
Wang C(王春)
;
Peng J(彭俊)
;
Jiang ZL(姜宗林)
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Submit date:2022/01/12
Hysteresis of Shock Train Movement in the Isolator with a Ramp
期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
Authors:
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang P
;
Zhao QJ
Adobe PDF(2961Kb)
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Submit date:2022/02/17
External-Compression Supersonic Inlet Free from Violent Buzz
期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
Authors:
Chen H
;
Tan H
;
Liu YZ
;
Zhang QF(张启帆)
Adobe PDF(4679Kb)
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Submit date:2019/09/09
Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows
期刊论文
AIAA JOURNAL, 2018, 卷号: 56, 期号: 8, 页码: 3086-3096
Authors:
Lee YC(李亚超)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(1783Kb)
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Submit date:2018/10/19
High-Pressure Capturing Wing Configurations
期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
Authors:
Cui K(崔凯)
;
Li GL
;
Xiao Y(肖尧)
;
Xu YZ
;
Cui,K(reprint author), Chinese Acad Sci, Inst Mech
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Submit date:2017/07/24
Investigations of Three-Dimensional Shock/Shock Interactions over Symmetrical Intersecting Wedges
期刊论文
AIAA JOURNAL, 2016, 卷号: 54, 期号: 5, 页码: 1472-1481
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Wang, C (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
Ceramics
Thermal Shock
Size Effect