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Zhengtao Guo

national university of defense technology

H指数:8

被引数:206

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Flow mechanism-embedded deep learning for modeling geometric uncertainty effects on aerodynamic stability

流动机理嵌入的深度学习用于模拟几何不确定性对气动稳定性的影响

Aerospace Science and Technology

IF5.8

2026-08-010

PRE

Secondary combustion steam reforming unlocks boron combustion potential in solid rocket scramjets

固体火箭超燃冲压发动机中二次燃烧蒸汽重整释放硼燃烧潜力

Acta Astronautica

IF3.4

2026-07-010

PRE

Theoretical study on the primary combustion of the boron-based fuel-rich propellant for solid rocket scramjet

Aerospace Science and Technology

IF5.8

2026-01-300

PRE

High-Fidelity Quantification of Manufacturing-Induced Uncertainty in Supersonic Flow Fields via Deep Autoencoder and Spatially-Adaptive Polynomial Chaos

Aerospace Science and Technology

IF5.8

2026-01-300

PRE

Research on compressor slotted stator based on multi-objective optimization and shapley additive exPlanation (SHAP) method

基于多目标优化和Shapley加性解释（SHAP）方法的压缩机槽式定子研究

Aerospace Science and Technology

IF5.8

2025-10-250

PRE

An efficient sparse surrogate model for aerodynamic characteristics of a supersonic compressor cascade with uncertain geometric deformations

几何变形不确定的超音速压气机叶栅气动特性的有效稀疏代理模型

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2024-07-016

PRE

Novel data-driven sparse polynomial chaos and analysis of covariance for aerodynamics of compressor cascades with dependent geometric uncertainties

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2024-06-012

OAAI

Extraction of geometric features and analysis of flow mechanism of high loaded compressor airfoils at low Reynolds number

PHYSICS OF FLUIDS

IF4.3

2024-03-220

OA

Statistical evaluation of stability margin of a multi-stage compressor with geometric variability using adaptive polynomial chaos-Kriging model

PHYSICS OF FLUIDS

IF4.3

2023-07-1314

PRE

Flow control mechanism of compressor cascade: A new leading-edge tubercles profiling method based on sine and attenuation function

PHYSICS OF FLUIDS

IF4.3

2023-06-089

PRE

Aerodynamic evaluation of cascade flow with actual geometric uncertainties using an adaptive sparse arbitrary polynomial chaos expansion

PHYSICS OF FLUIDS

IF4.3

2023-03-2117

PRE

A data-driven non-intrusive polynomial chaos for performance impact of high subsonic compressor cascades with stagger angle and profile errors

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2022-10-0134

PRE

Effect of span range of variable-camber inlet guide vane in an axial compressor

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2021-09-0114

PREAI