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Keywords

compressor, detached eddy simulation

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Employment (1)

Northwestern Polytechnical University: Xi'an, CN

2024-09-24 to present | Prof. (School of Power and Energy)
Employment
Source: Self-asserted source
Ruiyu Li

Education and qualifications (1)

Northwestern Polytechnical University: Xi'an, Shaanxi, CN

2014-09-01 to 2020-07-08 | PH.D Student (School of Power and Energy)
Education
Source: Self-asserted source
Ruiyu Li

Funding (1)

China Postdoctoral Science Foundation

Grant
China Postdoctoral Science Foundation (Beijing, CN)
GRANT_NUMBER:

263917
Source: Self-asserted source
Ruiyu Li

Works (11)

Twist Angle Error Statistical Analysis and Uncertain Influence on Aerodynamic Performance of Three-Dimensional Compressor Rotor

Aerospace
2024-07 | Journal article | Author
DOI: 10.3390/aerospace11080614
Contributors: Yue Dan; Ruiyu Li; Limin Gao; Huawei Yu; Yuyang Hao
Source: check_circle
Multidisciplinary Digital Publishing Institute

Study on the Tip Leakage Loss Mechanism of a Compressor Cascade Using the Enhanced Delay Detached Eddy Simulation Method

Entropy
2024-03 | Journal article | Author
DOI: 10.3390/e26040295
Contributors: Shiyan Lin; Ruiyu Li; Limin Gao
Source: check_circle
Multidisciplinary Digital Publishing Institute

Accuracy Investigations of Dynamic Characteristic Predictions of Tip Leakage Flow Using Detached Eddy Simulation

Aerospace
2023-12 | Journal article | Author
DOI: 10.3390/aerospace11010029
Contributors: Shiyan Lin; Ruiyu Li; Limin Gao; Ning Ge
Source: check_circle
Multidisciplinary Digital Publishing Institute

Influence of leading edge with real manufacturing error on aerodynamic performance of high subsonic compressor cascades

Chinese Journal of Aeronautics
2021-06 | Journal issue or edition
DOI: 10.1016/j.cja.2020.08.018
Part of ISSN: 1000-9361
Source: Self-asserted source
Ruiyu Li

Experimental Investigation of a Linear Cascade with Large Solidity Using Pressure Sensitive Paint and Dual-Camera System

Journal of Thermal Science
2021-03 | Journal issue or edition
DOI: 10.1007/s11630-021-1425-4
Part of ISSN: 1003-2169
Part of ISSN: 1993-033X
Source: Self-asserted source
Ruiyu Li

Corner separation dynamics in a high-speed compressor cascade based on detached-eddy simulation

Aerospace Science and Technology
2020-04 | Journal issue or edition
DOI: 10.1016/j.ast.2020.105730
Part of ISSN: 1270-9638
Source: Self-asserted source
Ruiyu Li

Dominating Unsteadiness Flow Structures in Corner Separation Under High Mach Number

AIAA Journal
2019-07 | Journal issue or edition
DOI: 10.2514/1.j057783
Part of ISSN: 0001-1452
Part of ISSN: 1533-385X
Source: Self-asserted source
Ruiyu Li

Application of shear-sensitive liquid crystal coating to visualization of transition and reattachment in compressor cascade

Chinese Journal of Aeronautics
2018-11 | Journal article
DOI: 10.1016/j.cja.2018.06.003
Part of ISSN: 1000-9361
Source: Self-asserted source
Ruiyu Li

Experimental investigation on static/dynamic characteristics of a fast-response pressure sensitive paint

Chinese Journal of Aeronautics
2018-06 | Journal issue or edition
DOI: 10.1016/j.cja.2018.04.006
Part of ISSN: 1000-9361
Source: Self-asserted source
Ruiyu Li

Optical Pressure Measurement Principle System

New Trends and Developments in Metrology
2016-04-28 | Book chapter
DOI: 10.5772/64008
Source: Self-asserted source
Ruiyu Li

Unsteady Investigation on Tip Flow Field and Rotating Stall in Counter-Rotating Axial Compressor

Journal of Engineering for Gas Turbines and Power
2015-07-01 | Journal issue or edition
DOI: 10.1115/1.4029101
Part of ISSN: 0742-4795
Part of ISSN: 1528-8919
Source: Self-asserted source
Ruiyu Li
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