Improved k-ω-γ model for crossflow-induced transition prediction in hypersonic flow L Zhou, R Li, Z Hao, DI Zaripov, C Yan
International Journal of Heat and Mass Transfer 115, 115-130, 2017
50 2017 Improved k–ω–γ model for hypersonic boundary layer transition prediction L Zhou, C Yan, ZH Hao, RF Du
International Journal of Heat and Mass Transfer 94, 380-389, 2016
48 2016 Spatial direct numerical simulation of the hypersonic boundary-layer stabilization using porous coatings R Zhao, CY Wen, TH Long, XD Tian, L Zhou, Y Wu
AIAA Journal 57 (11), 5061-5065, 2019
42 2019 Improved γ-Reθt model for heat transfer prediction of hypersonic boundary layer transition Z Hao, C Yan, Y Qin, L Zhou
International Journal of Heat and Mass Transfer 107, 329-338, 2017
35 2017 Full blended blade and endwall design of a compressor cascade M Tongtong, Y Guang, Z Ling, JI Lucheng
Chinese Journal of Aeronautics 34 (11), 79-93, 2021
28 2021 A laminar kinetic energy transition model appropriate for hypersonic flow heat transfer YP Qin, C Yan, ZH Hao, L Zhou
International Journal of Heat and Mass Transfer 107, 1054-1064, 2017
27 2017 Use of Blended Blade and End Wall method in compressor cascades: Definition and mechanism comparisons J Li, X Li, L Ji, W Yi, L Zhou
Aerospace Science and Technology 92, 738-749, 2019
26 2019 A combined criteria-based method for hypersonic three-dimensional boundary layer transition prediction L Zhou, R Zhao, R Li
Aerospace Science and Technology 73, 105-117, 2018
26 2018 Application of Improved L Zhou, R Zhao, W Yuan
AIAA Journal 57 (5), 2214-2221, 2019
25 2019 Transition model and transition criteria for hypersonic boundarylayer flow L Zhou, C Yan, Z Hao, W Kong, Y Zhou
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 37 (4), 1092-1102, 2016
21 2016 Development of a boundary layer parameters identification method for transition prediction with complex grids Z Hao, C Yan, L Zhou, Y Qin
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2017
19 2017 Effect of blended blade tip and winglet on aerodynamic and aeroacoustic performances of a diagonal fan C Zhang, L Ji, L Zhou, S Sun
Aerospace Science and Technology 98, 105688, 2020
18 2020 Design optimization of a blended blade and endwall in a compressor cascade J Li, L Ji, L Zhou
Journal of Engineering for Gas Turbines and Power 142 (2), 021003, 2020
18 2020 Large eddy simulation and combined control of corner separation in a compressor cascade T Meng, X Li, L Zhou, H Zhu, J Li, L Ji
Physics of Fluids 34 (7), 2022
17 2022 Corner stall control in linear compressor cascade by blended blade and endwall technique based on large eddy simulation JL Zhu Huiling, Zhou Ling, Meng Tongtong
Physics of Fluids 33 (11), 115124, 2021
17 2021 An investigation of interface conditions inherent in detached-eddy simulation methods L Zhou, R Zhao, W Yuan
Aerospace Science and Technology 74, 46-55, 2018
17 2018 转捩模式与转捩准则预测高超声速边界层流动 周玲， 阎超， 郝子辉， 孔维萱， 周禹
航空学报 37 (4), 1092-1102, 2016
15 2016 Influence of sub boundary layer vortex generator height and attack angle on cross-flows in the hub region of compressors FU Hao, Z Ling, JI Lucheng
Chinese Journal of Aeronautics 35 (8), 30-44, 2022
14 2022 Effect of a blade end slot on supersonic compressor cascade hub-corner separation J Ma, G Yang, L Zhou, L Ji, C Zhang
Aerospace Science and Technology 118, 107032, 2021
14 2021 CFD design of ventilation system for large underground bus terminal in Macau Barrier Gate R Zhao, L Zhou, J Ma
Journal of Wind Engineering and Industrial Aerodynamics 179, 1-13, 2018
14 2018 
Dinar ZaripovKutateladze Institute of Thermophysics, Siberian Branch of the RASΗ διεύθυνση ηλεκτρονικού ταχυδρομείου έχει επαληθευτεί στον τομέα itp.nsc.ru
