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Xiaoquan Yang

Shanghai University

H指数:8

被引数:233

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Experimental and numerical investigations of the flow control mechanism with combined spike-porous jet techniques in hypersonic flow

高超声速流中结合尖楔-多孔喷射技术的流动控制机制的实验与数值研究

International Communications in Heat and Mass Transfer

IF6.4

2026-03-110

PRE

Noise Control of Swept High-Lift Devices Using Slat Cove Wavy Wall

利用襟翼凹槽波纹壁对后掠高升力装置的噪声控制

Aerospace Science and Technology

IF5.8

2026-02-200

PRE

Data-Parallel Right-Updating Algorithm for the Discontinuous Galerkin Method in Compressible Viscous Flow

Journal of Aerospace Engineering

IF1.6

2025-11-010

PRE

Aeroacoustics evaluation and mechanism of Krueger flap

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2025-06-010

PRE

Analysis of geometrical parameter sensitivity and mechanism of flow loss in exhaust volute based on particle swarm optimization

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2025-02-010

PRE

An experimental study of noise generated by tandem blades

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2025-02-010

OAAI

Numerical simulation of aerodynamic noise characteristics of square-wave cylinder at Reynolds number 3900

PHYSICS OF FLUIDS

IF4.3

2025-01-070

PRE

Efficiency high-order discontinuous Galerkin method for low speeds flows with time-derivative preconditioning

PHYSICS OF FLUIDS

IF4.3

2024-10-180

PRE

Azimuthally-distributed wavy inner wall treatment for high subsonic jet noise control

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2024-10-010

OAAI

Noise control for nose landing gear by longitudinal wavy strut

纵向波浪形支柱对前起落架噪声的控制

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2024-09-010

PRE

Prediction of mean flow and over-tip shock distribution in pressure-driven tip leakage flows

PHYSICS OF FLUIDS

IF4.3

2024-01-112

PRE

Noise reduction for high-lift devices on a swept wing model by droop nose

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2023-12-012

PRE

A robust compact least-squares reconstruction method for compressible turbulent flow simulations of complex configurations

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2023-12-013

OAAI

Numerical investigation on flow and heat transfer mechanism of corrugated cooling channel in turbine blades

PHYSICS OF FLUIDS

IF4.3

2023-02-0118

PRE

Effects of slat track on the flow and acoustic field of high-lift devices

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2022-07-017

PRE

A method for the reconstruction of buzz-saw noise source and pressure field in transonic fan with multi-types of blade variations

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2022-07-012

PRE

Numerical study on the flow and noise control mechanism of wavy cylinder

PHYSICS OF FLUIDS

IF4.3

2022-03-1123

PRE

Noise control for high-lift devices by slat wall treatment

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2021-08-0122

PREAI

Operational mode transition in a rotating detonation engine

旋转爆震发动机的工作模式转换

zhejiang university science b

IF3.9

2020-10-2014

PREAI

Performance of rotating detonation engine with stratified injection

分层喷射旋转爆震发动机的性能

zhejiang university science b

IF3.9

2020-10-209

PREAI