He has published about 100 peer-reviewed papers. 

Selected journal articles (*corresponding author):

[1]    Liu Yangwei*, Tang Yumeng, Liu Baojie, Lu Lipeng, An Exponential Decay Model for the Deterministic Correlations in Axial Compressors, ASME Journal of Turbomachinery, 2018, online.     DOI: 10.1115/1.4041380

[2]    Xie zhe, Liu Yangwei*, Liu Xiaohua, Lu Lipeng, Sun Xiaofeng, Effect of RANS Method on the Stall Onset Prediction by an Eigenvalue Approach, ASME Journal of Fluids Engineering, 2018, online. DOI: 10.1115/1.4041362.

[3]    Tang Yumeng, Liu Yangwei*, Lu Lipeng, Solidity Effect on Corner Separation and Its Control in a High-Speed Low Aspect Ratio Compressor Cascade, International Journal of Mechanical Sciences, 2018, 142: 304-321.

[4]    Yan Hao, Liu Yangwei*, Li Qiushi, Lu Lipeng, Turbulence Characteristics in Corner Separation in a Highly Loaded Linear Compressor Cascade, Aerospace Science and Technology, 2018, 75: 139-154.

[5]    Muhammad Afzaal Asghar, Liu Yangwei*, Cui Jiahuan, Lu Lipeng*, Investigation of Unsteady Flow Interactions in a Transonic High Pressure Turbine Using Nonlinear Harmonic Method, Energies, 2018, 11: 342.

[6]    Xie zhe, Liu Yangwei*, Liu Xiaohua, Sun Dakun, Lu Lipeng, Sun Xiaofeng,  Computational Model for Stall Inception and Nonlinear Evolution in Axial Flow Compressors, AIAA Journal of Propulsion and Power, 2018, 34(3): 720-729.

[7]    Liu Yangwei, Yan Hao, Lu Lipeng*, Li Qiushi, Investigation of Vortical Structures and Turbulence Characteristics in Corner Separation in a Linear Compressor Cascade Using DDES, ASME Journal of Fluids Engineering, 2017, 139(2): 021107.

[8]    Gao Feng, Ma Wei, Sun Jinjing, Boudet Jérôme, Ottavy Xavier, Liu Yangwei*, Lu Lipeng, Shao Liang, Parameter Study on Numerical Simulation of Corner Separation in LMFA-NACA65 Linear Compressor Cascade, Chinese Journal of Aeronautics, 2017, 30(1): 15–30.

[9]    Fang Le, Zhao Hong-kai, Lu Li-peng*, Liu Yang-wei, Yan Hao, Quantitative Description of Non-Equilibrium Turbulent Phenomena in Compressors, Aerospace Science and Technology, 2017, 71: 78~89.

[10] Liu Yangwei*, Sun Jinjing, Tang Yumeng, Lu Lipeng, Effect of Slot at Blade Root on Compressor Cascade Performance under Different Aerodynamic Parameters, Applied Sciences. 2016, 6(12): 421.

[11] Liu Yangwei, Yan Hao, Fang Le*, Lu Lipeng, Li Qiushi, Shao Liang, Modified k-ω Model Using Kinematic Vorticity for Corner Separation in Compressor Cascade, Science China Technological Sciences, 2016, 59(5): 795-806.

[12] Liu Yangwei, Yan Hao, Liu Yingjie*, Lu Lipeng, Li Qiushi, Numerical Study of Corner Separation in a Linear Compressor Cascade Using Various Turbulence Models, Chinese Journal of Aeronautics, 2016, 29(3): 639–652.

[13] Liu Yangwei, Yan Hao* and Lu Lipeng, Numerical Study of the Effect of Secondary Vortex on Three-Dimensional Corner Separation in a Compressor Cascade, International Journal of Turbo & Jet-Engines, 2016, 33(1): 9-18.

[14] Liu Yangwei, Wu Jianuo, Lu Lipeng*, Performance of Turbulence Models for Transonic Flows in a Diffuser, Modern Physics Letters B, 2016, 30(25): 1650326.

[15] Lu Lipeng, Zhong Luyang, Liu Yangwei*, Turbulence Models Assessment for Separated Flows in a Rectangular Asymmetric Three-Dimensional Diffuser, Engineering Computations, 2016, 33(4): 978-994.

[16] Fang Le, Sun Xueyan, Liu Yangwei *, A Criterion of Orthogonality on the Assumption and Restrictions in Subgrid-Scale Modelling of Turbulence, Physics Letters A, 2016, 380(47): 3988–3992.

[17] Gao Yanfei, Liu Yangwei*, Zhong Luyang, Hou Jiexuan, LuLipeng, Study of the Standard k-ε Model for Tip Leakage Flow in an Axial Compressor Rotor, International Journal of Turbo & Jet-Engines, 2016, 33(4): 353–360.

[18] Fang Le, Zhu Ying, Liu Yangwei*, Lu Lipeng, Spectral Non-Equilibrium Property in Homogeneous Isotropic Turbulence and Its Implication in Subgrid-Scale Modeling, Physics Letters A, 2015, 379(38): 2331–2336.

[19] Liu Baojie, Zhang bo, Liu Yangwei*, Investigation of Model Development for Deterministic Correlations Associated with Impeller-Diffuser Interactions in Centrifugal Compressors, Science China Technological Sciences, 2015, 58(3): 499–509.

[20] Liu Yangwei, Sun Jinjing*, Lu Lipeng, Corner Separation Control by Boundary Layer Suction Applied to a Highly Loaded Axial Compressor Cascade,Energies, 2014, 7(12): 7994-8007.

[21] Liu Baojie, Zhang bo, Liu Yangwei*, Numerical Investigations of Impeller-Diffuser Interaction in a Transonic Centrifugal Compressor Stage Using Nonlinear Harmonic Method, Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2014, 228(8): 862–877.

[22] Liu Yang-Wei*, Liu Bao-Jie, Lu Li-Peng, Study of Modeling Unsteady Blade Row Interaction in a Transonic Compressor Stage Part 1: Code Development and Deterministic Correlations Analysis, Acta Mechanica Sinica, 2012, 28(2): 281-290.

[23]  Liu Yang-Wei*, Liu Bao-Jie, Lu Li-Peng, Study of Modeling Unsteady Blade Row Interaction in a Transonic Compressor Stage Part 2: Influence of Deterministic Correlations on Time-averaged Flow Prediction, Acta Mechanica Sinica, 2012, 28(2): 291-299.

[24] Liu Yangwei*, Lu Lipeng, Fang Le, Gao Feng, Modification of Spalart-Allmaras Model with Consideration of Turbulence Energy Backscatter Using Velocity Helicity, Physics Letters A, 2011, 375(24): 2377-2381.

[25] Liu Yangwei*, Yu Xianjun, Liu Baojie, Turbulence Models Assessment for Large-Scale Tip Vortices in an Axial Compressor Rotor, AIAA Journal of Propulsion and Power, 2008, 24(1): 15-25.

[26] Hou Jiexuan, Liu Yangwei*, Lu Lipeng. Effects of moving endwall on tip leakage flow in compressor cascade. Journal of Aerospace Power, 2018, 33(4): 803-811. (in Chinese)

[27] Ge Jian, Liu Yangwei*, Lu Lipeng, Effects of Casing Temperature Boundary Condition on Performance of a Transonic Rotor. Journal of Propulsion Technology, 2018, 39(7): 1486-1493. (in Chinese)

[28] Gao Yanfei, Liu Yangwei*, Lu Lipeng. Modification of Realizable k-ε Model for Tip-leakage Flow in an Axial Compressor Rotor. Journal of Engineering Thermophysics, 2018, accepted. (in Chinese)

[29] Zhong Luyang, Liu Yangwei*, Lu Lipeng, Investigation of Tip Leakage Flow in a Compressor Rotor Using DDES. Journal of Engineering Thermophysics, 2018, accepted. (in Chinese)

[30] Ge Jian, Liu Yangwei*, Zhou Zhenhua, Lu Lipeng, Title. Journal of Engineering Thermophysics, 2018, accepted. (in Chinese)

[31] Tang Yumeng, Liu Yangwei*, Lu Lipeng, Performance of the High-Speed Conventional Loading Cascade Influenced by the Blade End Slots. Journal of Engineering Thermophysics, 2018, accepted. (in Chinese)

[32] Sun Jinjing, Liu Yangwei*, Lu Lipeng, Ottavy Xavier. Control of Corner Separation by Slot at the Root of the Blade. Journal of Engineering Thermophysics, 2017, accepted. (in Chinese)

[33] Tang Yumeng, Liu Yangwei*, Lu Lipeng, Lu Huawei. Experimental Investigation of Losses in a High-Speed High-Loading Compressor Cascade. Journal of Engineering Thermophysics, 2017, 38(8): 1624-1633. (in Chinese)

[34] Wu Jianuo, Lu LiPeng, Liu YangWei*, Performance Evaluation of Turbulence Models for Complex Flows in Sajben Diffuser, Journal of Aerospace Power, 2017, 32(5): 1216-1223. (in Chinese)

[35] Wang Jing, Yong Xiaosong, Liu YangWei*, Lu LiPeng, Performance Study of the Turbulence Models in a Two-Dimensional U-Bend Duct. Journal of Engineering Thermophysics, 2017, 38(4): 710-718. (in Chinese)

[36] Tang Yumeng, Liu YangWei*, Lu LiPeng, Evaluation on Turbulence Models in Simulating Complex Flows Around High-Lift Airfoil, Journal of Aerospace Power, 2016, 31(12): 2859-2869. (in Chinese)

[37] Duan Zhenzhen, Liu YangWei*, Lu LiPeng, Effects of Tip Clearance Size on Flowfield in a Low-Speed Axial Compressor Rotor, Applied Mechanics and Materials, 2014, 543-547: 158-163.

[38] Yan Hao, Liu Yangwei*, Fang Le, Lu Lipeng, Modification of Spalart-Allmaras Turbulence Model for Predicting S825 Airfoil Aerodynamic Performance, Applied Mechanics and Materials, 2014, 543-547: 189-194.

[39] Fang Le*, Wu Jianzhao, and Liu Yangwei, Inverse SPH Method: a New Method for Restoring High-Order Consistency, Energy Education Science and Technology Part A: Energy Science and Research, 2014, 32(6): 4839-4848.

[40] Yan Hao, Liu Yangwei*, Lu Lipeng, The Effects of Secondary Flow on 3-D corner separation in compressor cascade, Journal of Engineering Thermophysics, 2014, 35(6): 1075-1078. (in Chinese)

[41] Duan Zhenzhen, Liu Yangwei*, Lu Lipeng, Influence of Circumferential Casing Grooves on Transonic Compressor Rotor Performance, Acta Aeronautica ET Astronautica Sinica, 2014, 35(8): 2163-2173. (in Chinese)

[42] Sun Jinjing, Liu Yangwei*, Lu Lipeng, Control of Corner Separation to Enhance Stability in a Linear Compressor Cascade by Boundary Layer Suction, Procedia Engineering, 2014, 80: 380- 391; or The 3rd International Symposium on Aircraft Airworthiness (ISAA 2013), ENAC Toulouse (France), November 19-21, 2013.

[43] Cui Jian, Zhao Bin, Liu Yangwei, Li Shaobin, Numerical Research on the Safety and Performance of Transonic Compressor with Bleed Air at Multiple Operation State. Procedia Engineering, 2014, 80: 352-364; or The 3rd International Symposium on Aircraft Airworthiness (ISAA 2013), ENAC Toulouse (France), November 19-21, 2013.

[44] Luo Tianpei, Liu Yangwei*, Lu Lipeng, Transition Model Assessment and Modification in Low-Pressure Turbine Cascade. Acta Aeronautica ET Astronautica Sinica, 2013, 34(7): 1548-1562. (in Chinese)

[45] Wen Xiaoqing, Liu Yangwei, Fang Le, Lu Lipeng, Improving the Capability of k-ω SST Turbulence Model for Predicting Stall Characteristics of Airfoil. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(8): 1127-1132. (in Chinese)

[46] Fang Le*, Liu Yangwei, Jing Guoqing, Huang Shujun, Review of Some Recent Patents on the Large-Eddy Simulation Technique in Turbulence, Recent Patents on Mechanical Engineering, 2012, 5(2): 89-95.

[47] Zhang Bo, Liu Yangwei*, Liu Baojie, Numerical Simulation of Low Engine Order Excitation in a Transonic Compressor, Advanced Materials Research, 2012, 546-547: 206-211.

[48] Zhou Dagao, Liu Yangwei, Wen Xiaoqing, Lu Lipeng, Modification of SA model for predicting airfoil flow separation, Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(10): 1384-1388. (in Chinese)

[49] Liu Yangwei*, Liu Baojie, Numerical Investigation of Impeller-Diffuser Interaction in a Centrifugal Compressor, Journal of Aerospace Power, 2009, 24(12): 2695-2702. (in Chinese)

[50] Liu Yangwei*, Huang Weibing, Liu Baojie, Analysis of Deterministic Stresses in a Centrifugal Compressor, Journal of Aerospace Power, 2008, 23(3): 534-540. (in Chinese)

[51] Liu Yangwei*, Liu Baojie, Assessment of Turbulence Models for the Prediction of Large-Scale Tip Vortices in an Axial Compressor Rotor, Journal of Engineering Thermophysics, 2008, 29(3): 399-402. (in Chinese)

[52] Liu Yangwei, Liu Baojie*, Analysis of Deterministic Stresses in a Transonic Compressor, Acta Aeronautica ET Astronautica Sinica, 2007, 28(Sup): 1-6. (in Chinese)

[53] Zhao Jun, Liu Yangwei, Liu Baojie, Frequency-Domain Analysis of NASA67 Unsteady Flow Field, Journal of Aerospace Power, 2007, 22(8): 1371-1377. (in Chinese)

[54] Sun Jinijng., Liu Yangwei*, Lu Lipeng, Ottavy Xavier, Control of Corner Separation by Optimized Slot Configuration in a Linear Compressor Cascade, Compressor Blower & Fan Technology, 2016,6: 9-18.

Selected conference proceedings papers (*corresponding author): 

[55] Liu Yangwei*, Zhong Luyang, Lu Lipeng, Comparison of DDES and URANS for Unsteady Tip Leakage Flow in an Axial Compressor Rotor, ASME Turbo Expo. 2018, GT2018-76487, Oslo, Norway, June 11-15, 2018.

[56] Muhammad Afzaal Asghar, Liu Yangwei*, Lu Lipeng. Numerical investigation of unsteady flow interactions in a transonic single stage high pressure turbine. 15th International Bhurban Conference on Applied Sciences and Technology (IBCAST), Islamabad, Pakistan , Jan, 9-13, 2018.

[57] Xie Zhe, Liu Yangwei*, Liu Xiaohua, Lu Lipeng, Sun Xiaofeng, Effect of RANS Method on Stall Inception Eigenvalue Approach, ASME Turbo Expo. 2017, GT2017-64708, Charlotte, North Carolina, USA, June 26–30, 2017.

[58] Muhammad Afzaal Asghar, Lu Lipeng, Liu Yangwei, Su Zhi, Numerical Investigation of Secondary Flows Through Highly Loaded Transonic Turbine Stage, 14th International Bhurban Conference on Applied Sciences and Technology (IBCAST), Islamabad , Pakistan , 2017.

[59] Liu Yangwei, Yan Hao*, Lu Lipeng, Investigation of Corner Separation in a Linear Compressor Cascade Using DDES, ASME Turbo Expo. 2015, GT2015-42902, Montréal, Canada, June 15-19, 2015.

[60] Duan Zhenzhen, Liu Yangwei*, Lu Lipeng, Numerical Investigation of the Behavior of Tip Leakage Flow in a Low-speed Axial Compressor Rotor at Near-Stall Condition, ASME Turbo Expo. 2012, GT2012-69635, Copenhagen, Denmark, June 11-15, 2012.

[61] Liu Yangwei*, Liu Baojie, Lu Lipeng, Investigation of Unsteady Impeller-Diffuser Interaction in a Transonic Centrifugal Compressor Stage, ASME Turbo Expo. 2010, GT2010-22737, Glasgow, UK, June 14-18, 2010.

 [62] Zhong Luyang, Liu Yangwei*, Lu Lipeng, Unsteady Behavior of Tip Leakage Vortex in an Axial Compressor with Different Rotor Tip-Gap Sizes using DDES, The Third Chinese International Turbo-machinery Conference, NO.201802340, April 12-15, 2018, Chongqing, China.

[63] Liu Yangwei*, Liu Baojie, Lu Lipeng. An Exponential Decay Model for the Deterministic Correlations in Axial Compressors, The 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, December 16-21 2017, Hawaii, Maui, USA.

[64] Tang Yumeng, Liu Yangwei*, Lu Lipeng, Lu Huawei, Wang Ming. Experimental Investigation of Flow Control Using Blade End Slots in a Highly Loaded Compressor Cascade. The 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, December 16-21 2017, Hawaii, Maui, USA.

[65] Liu Yangwei*, Zhong Luyang, Lu Lipeng. Investigation of Flow Structures and Unsteady Characteristics in Tip Leakage Flow in a Compressor Rotor Using DDES, The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering, NO.170762, Nov 20-23, 2017, Beijing, China.

[66] Liu Yangwei*, Zhong Luyang, Lu Lipeng. Study of Tip Leakage Flow Prediction Using the Quadratic Constitutive Relation, The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering, NO.170763, Nov 20-23, 2017, Beijing, China.

[67] Gao Yanfei, Liu Yangwei*, Lu Lipeng. A Flow Model for Tip Leakage Flow in Turbomachinery Using a Planar Duct with a Longitudinal Slit, The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering, NO.170764, Nov 20-23, 2017, Beijing, China.

[68] Gao Yanfei, Liu Yangwei*, Lu Lipeng. Modification of Realizable k-ε Model for Tip Leakage Flow in an Axial Compressor Rotor, The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering, NO.170765, Nov 20-23, 2017, Beijing, China.

[69] Liu Yangwei, Yong Xiaosong, Yan Hao*, Lu Lipeng. Delay Detached Eddy Simulation of Separation Flows in a Three-Dimensional U-duct, The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering, NO.170766, Nov 20-23, 2017, Beijing, China.

[70] Liu Yangwei, Yong Xiaosong, Yan Hao*, Lu Lipeng. Numerical Study of Flow in a Two-Dimensional U-Duct using Various Turbulence Models, The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering, NO.170767, Nov 20-23, 2017, Beijing, China.

[71] Liu Yangwei*, Sun Jinjing, Lu Lipeng, Control of Corner Separation in a Linear Highly Loaded Compressor Cascade by Boundary Layer Suction, 3rd Symposium on FSSIC, No.A117, Perth, Western Australia, 5th-9th July, 2015.    

[72] Gao Yanfei, Liu Yangwei*, Zhong Luyang, Hou Jiexuan, Lu Lipeng, Study of the k-ε Model for Tip Leakage Flow in an Axial Compressor Rotor, Proceedings of 2015 Asian-Pacific Conference on Aerospace Technology and Science, No.140191, May 20-23, 2015, Jeju Island, Korea.

[73] Zhong Luyang, Liu Yangwei*, Gao Yanfei, Hou Jiexuan, Lu Lipeng, Modification of SA Model with Consideration of Turbulence Anisotropy for Tip Leakage Flow in an Axial Compressor Rotor, Proceedings of 2015 Asian-Pacific Conference on Aerospace Technology and Science, No.140180, Jeju Island, Korea, May 20-23, 2015.

[74] Hou Jiexuan, Liu Yangwei*, Zhong Luyang, Gao Yanfei, Lu Lipeng, Turbulence Models Assessment for Tip Leakage Flow through a Linear Compressor Cascade, Proceedings of 2015 Asian-Pacific Conference on Aerospace Technology and Science, No.140174, Jeju Island, Korea, May 20-23, 2015.

[75] Liu Yangwei, Yan Hao*, Lu Lipeng, Modifying k-ω Model with Consideration of Kinematic Vorticity on Predicting Corner Separation in Compressor Cascade, The 5th International Symposium on Jet Propulsion and Power Engineering, 2014-ISJPPE-5016, Beijing, China, September 15-19, 2014.

[76] Liu Yangwei*, Liu Baojie, Lu Lipeng, Implementation and Validation of the Spalart-Allmaras Turbulence Model in Transonic Compressor Flows, ASIAN CONGRESS ON GAS TURBINES 2012 (ACGT2012), ACGT2012-1056, Shanghai, August 20-22, 2012.

[77] Liu Baojie, Zhang bo, Liu Yangwei*, Numerical Investigation of Unsteady Tip Clearance Flow in a Low Speed Axial Compressor, ASIAN CONGRESS ON GAS TURBINES 2012 (ACGT2012), ACGT2012-1031, Shanghai, August 20-22, 2012.

[78] Liu Yangwei*, Liu Baojie, Lu Lipeng, Investigation of Deterministic Correlations in a Transonic Compressor Stage, ACFD0122-T008-A-001, The 8th Asian Computational Fluid Dynamics Conference, Hong Kong, 10-14 January, 2010.

[79] Lu Lipeng, Wang Danhua, Liu Yangwei*, Modification of S-A Model for Predicting Corner Separation Flows in Axial Compressor, ACFD0149-T008-A-001, The 8th Asian Computational Fluid Dynamics Conference, Hong Kong, 10-14 January, 2010.