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Influence of Non Uniform Bluntness on Aerodynamic Performance and Aerothermal Characteristics of Waverider
期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 3, 页码: 205
Authors:
Qu, Zhipeng
;
Wang, Wanyu
;
Xiao, Houdi
;
Xiao Y(肖尧)
;
Li GL(李广利)
;
Cui K(崔凯)
Adobe PDF(67504Kb)
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Submit date:2023/04/20
waverider
non uniform
hypersonic
computational fluid dynamics (CFD)
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle
期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(5479Kb)
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Submit date:2022/08/24
Multistage Launch Vehicle
Aerodynamic Characteristics
Shock Wave Interaction
Angle of Attack
Waverider
Boundary Layer Flow
Total Variation Diminishing
Adverse Pressure Gradient
Hypersonic Flows
Hypersonic Wind Tunnels
Gas-surface interactions in a large-scale inductively coupled plasma wind tunnel investigated by emission/absorption spectroscopy
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 8, 页码: 14
Authors:
Fang SH(方思晗)
;
Lin X(林鑫)
;
Zeng, Hui
;
Zhu, Xingying
;
Zhou, Fa
;
Yang JN(杨俊娜)
;
Li F(李飞)
;
Ou, Dongbin
;
Yu XL(余西龙)
Adobe PDF(5914Kb)
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Submit date:2022/09/16
基于多层分块算法的激波干扰流场预测
期刊论文
力学学报, 2021, 卷号: 53, 期号: 12, 页码: 3284-3297
Authors:
李帅
;
彭俊
;
罗长童
;
胡宗民
Adobe PDF(2372Kb)
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Submit date:2022/03/16
激波干扰
高温气体效应
多层分块算法
高超声速流动
气动热
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV
期刊论文
Advances in Aerodynamics, 2021, 卷号: 3, 期号: 1
Authors:
Qi H(齐涵)
;
Li XL(李新亮)
;
Yu ZP(于长平)
;
Tong FL(童福林)
Adobe PDF(4454Kb)
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Submit date:2021/11/01
Lifting body model
Hypersonic transition
Direct numerical simulation
Numerical study on aerodynamic performance of waverider with a new bluntness method
期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233
Authors:
Qu ZP
;
Xiao HD
;
Lv MY
;
Li GL(李广利)
;
Cui K(崔凯)
Adobe PDF(1179Kb)
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Submit date:2021/06/11
bluntness method
computational fluid dynamics
hypersonic
volume
Waverider
Evolution of heat transfer at the stagnation point during the detached bow shock establishment
期刊论文
SHOCK WAVES, 2021, 页码: 8
Authors:
Wang Q(汪球)
;
Li JP(李进平)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Zhao W(赵伟)
Adobe PDF(1158Kb)
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Submit date:2021/05/17
Hypersonic
Aerodynamic heating
Detached bow shock
Shock tube
expansion tube
Parameter-correlation study on shock-shock interaction using a machine learning method
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors:
Peng J(彭俊)
;
Luo ZT(罗长童)
;
Han ZJ(韩子健)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
Adobe PDF(2818Kb)
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Submit date:2021/01/29
Shock-shock interaction
Machine learning
Hypersonic flow
Impinging jet
Genetic programming
Triple point
Nonprobabilistic uncertain model updating and optimization design of thermal protection system
期刊论文
APPLIED THERMAL ENGINEERING, 2020, 卷号: 180, 页码: 14
Authors:
Jiang WT
;
Wang XJ
;
Wang RX(王睿星)
;
Shi QH
;
Zhu JJ
Adobe PDF(6028Kb)
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Submit date:2020/11/30
Thermal protection system
Nonprobabilistic optimization
Sensitivity analysis
Uncertainty analysis
Model updating
传感器安装对平板气动热测量精度的影响
期刊论文
北京航空航天大学学报, 2020, 卷号: 47, 期号: 09, 页码: 1790-1798
Authors:
罗凯
;
汪球
;
栗继伟
;
李进平
;
赵伟
Adobe PDF(2231Kb)
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Submit date:2021/11/12
平板
气动热
安装精度
雷诺数
边界层