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Xiaoge Lu

national university of defense technology - china

H指数:9

被引数:238

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Coupling effect of concave curvature and transpiration cooling film coverage in hypersonic flow

高超声速流中凹面曲率与发汗冷却薄膜覆盖的耦合效应

Aerospace Science and Technology

IF5.8

2026-08-260

PRE

Thermal Protection Characteristics of Annular Centripetal Film in Hypersonic Forward-Facing Cavity

超声速前向凹腔中环形离心薄膜的热防护特性

IF2.8

2026-05-010

PRE

Experimental and CFD investigation of the heat flux distribution and flow field structure on the leeward side of a 75∘ delta flat plate

实验与计算流体动力学(CFD)对75∘三角翼平板背风面热流分布及流场结构的探究

Aerospace Science and Technology

IF5.8

2025-09-200

PRE

Experimental investigation on mixing and thermal protection of jet cooling and transpiration cooling for rudder leading edge

对喷气冷却和渗流冷却在舵面前缘混合与热防护的实验研究

Applied Thermal Engineering

IF6.9

2025-08-260

PRE

Visualization and spatial evolution of streamwise vortices near the minor axis of an elliptical cone

椭圆锥小轴附近流向涡的可视化与空间演化

PHYSICS OF FLUIDS

IF4.3

2025-03-120

PRE

An experimental investigation of supersonic conical cooling films with angles of attack

PHYSICS OF FLUIDS

IF4.3

2024-10-011

PRE

An experimental study of supersonic conical cooling films subjected to different ratios of static pressure

PHYSICS OF FLUIDS

IF4.3

2024-08-162

PRE

Theoretical validation and experimental calibration of a variable Mach number tunnel with continuous wave-elimination

PHYSICS OF FLUIDS

IF4.3

2023-12-070

PRE

Hypervelocity imperfect gas nozzle design with shared wave-elimination contour

PHYSICS OF FLUIDS

IF4.3

2023-08-082

PRE

Novel design of variable Mach number nozzle operated by a single jack

PHYSICS OF FLUIDS

IF4.3

2023-07-050

OA

An experimental investigation on the isoenergetic supersonic cooling films subjected to different ratios of static pressure

PHYSICS OF FLUIDS

IF4.3

2023-05-1213

OA

Time-resolved visualization of coherent structures during supersonic boundary layer transition

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2023-04-016

OAAI

Experimental investigation of expansion effect on shock wave boundary layer interaction near a compression ramp

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2022-12-0111

OAAI

Experimental study of the high-frequency instability in the hypersonic boundary layer over a cone at 6° angle of attack

6 ° 攻角圆锥上高超声速边界层高频不稳定性的实验研究

ACTA MECHANICA SINICA

IF4.6

2022-07-122

PRE

Delaying hypersonic boundary layer transition using forward-facing step arrays: An experimental work

PHYSICS OF FLUIDS

IF4.3

2022-06-155

PRE

A swept fin-induced flow field with different height mounting gaps

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2021-01-0118

OAAI

Experimental investigation of boundary layer transition over a delta wing at Mach number 6

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2020-07-0128

OAAI