GPPS Xi’an21: Proceedings

  1. Analysis of Rotating Instability in Axial Compressor Based on Dynamic Mode Decomposition Bo Lian, Xiaocheng Zhu, Xiaojian Yang, Zhaohui Du (2022), DOI: DOI: 10.33737/gpps21-tc-9,

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  2. Effect Of Circumferential Single Casing Groove Location On The Flow Stability Under Tip Clearance Effect In A Transonic Axial Flow Compressor Rotor Xiaochen Mao*, Zonghao Yang, Xiaoxiong Wu, Bo Liu (2022), DOI: DOI: 10.33737/gpps21-tc-12,

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  3. Pressure Fluctuation Characteristics Of Mixed-Flow Pump Under Near Stall Condition Wei Li, Leilei Ji, Ling Zhou, Dele Lu, Ramesh K. Agarwal (0), DOI: DOI: 10.33737/gpps21-tc-16,

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  4. Stall Inception Analysis Of A Transonic Compressor Based On A Global Stability Method Xingao Xie, Zhengxian Liu, Xiaojian Li (2022), DOI: DOI: 10.33737/gpps21-tc-22,

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  5. Aerodynamic Improvement Of The 16-Stage Axial Compressor G.М. Popov, Oleg V. Baturin, V. M. Zubanov, M.G. Miheev, E. S. Goriachkin, V. O. Nepomnyaschiy, E. R. Fisher, A. K. Vorobyev (2022), DOI: DOI: 10.33737/gpps21-tc-33,

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  6. A Parametric Study Of Circumferential Range Of Inlet Distortions On Transonic Rotor Stall Process Guoming Zhu, Bo Yang, Moru Song, Shuyi Zhang, Hong Xie (2022), DOI: DOI: 10.33737/gpps21-tc-39,

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  7. Research of laws and prediction of axial-flow compressor characteristics based on data driven Tantao Liu, Limin Gao, Xudong Feng (2022), DOI: DOI: 10.33737/gpps21-tc-41,

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  8. Effect of Pulsed Endwall Injection on Flow Separation and Vortex Structure of a Compressor Cascade Zhiyuan Cao, Cheng Song, Xi Gao, Xiang Zhang (2022), DOI: 10.33737/gpps21-tc-46,

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  9. Analysis On The Spike-type Rotating Stall For Axial Compressor By Dynamic Mode Decomposition Moru Song, Bo Yang, Guoming Zhu, Shuyi Zhang, Hong Xie (2022), DOI: 10.33737/gpps21-tc-48,

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  10. Time-Resolved Mode Characteristics Of Rotating Instability And Rotating Stall In An Axial Compressor Yadong Wu*, Zeyuan Yang, Jie Tian, Ming Li, Hua Ouyang (2022), DOI: 10.33737/gpps21-tc-66,

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  11. A Method For The Characterization Of Fans Down To Zero Speed And Analysis Of Bypass Reverse Flow During Ground Ferran Roig Tió, Hasani Azamar, Vassilios Pachidis (2022), DOI: 10.33737/gpps21-tc-81,

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  12. Mechanism On The Interactions Of Rotor Tip Flow With Slot-Type Casing Treatment In A Transonic Compressor Stage Zhidong Chi, Wuli Chu, Yaofeng Zhang, Ziyun Zhang, Haoguang Zhang (2022), DOI: 10.33737/gpps21-tc-89,

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  13. Research On The Application Of Similarity Principle For Multistage Axial Compressor Hong Xie, Bo Yang, Shuyi Zhang, Moru Song, Guoming Zhu (2022), DOI: 10.33737/gpps21-tc-120,

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  14. The mechanism of axial arrangement affecting the performance for tandem rotor with partial-height booster rotor in high-throughflow fan Chuangxin ZHOU, Shengfeng ZHAO, Chengwu YANG, Ge HAN, Xingen LU (2022), DOI: 10.33737/gpps21-tc-123,

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  15. Influence of Surface Roughness on a Highly Loaded Axial Compressor Stage Performance at Low Reynolds Number Hongzhi Cheng, Mingyang Wang, Chuangxin Zhou, Shengfeng Zhao, Xingen Lu, Junqiang Zhu (2022), DOI: 10.33737/gpps21-tc-161,

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  16. Introduction Of An Improved Axial Compressor Profile Shape Modelling Approach For Increased Flexibility In Transonic Profile Design Marcel Seidler, Jens Friedrichs (2022), DOI: 10.33737/gpps21-tc-173,

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  17. The Effect of IGV Wake on Axial Compressor Rotor at Low Reynolds Numbers Lin Li, Yanfeng Zhang, Ge Han (2022), DOI: 10.33737/gpps21-tc-184,

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  18. A New Robust Regenerative Turbo-Reactor Concept For Clean Hydrocarbon Cracking Dylan Rubini *, Nikolas Karefyllidis *, Liping Xu, Budimir Rosic, Harri Johannesdahl (2022), DOI: 10.33737/gpps21-tc-210,

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  19. Blade Tip Signal Analysis Of An Axial Compressor Ruize Xu, Jia Li, Xu Dong, Dakun Sun, Xiaofeng Sun, Congcong Chen (2022), DOI: 10.33737/gpps21-tc-216,

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  20. Influence Of Leading Edge Erosion On The Performance Of Transonic Fan Blade Bowei Xue, Lei Shi, Xiuxian Li, Hongbo Peng, Long Ma, Qi Jiang (2022), DOI: 10.33737/gpps21-tc-237,

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  21. Geometry Scaling Technique For Aerodynamic Redesign Of Multistage Transonic Compressor Xiawen Zhang, Yaping Ju, Cong Li, Dejun Meng, Chuhua Zhang (2022), DOI: 10.33737/gpps21-tc-240,

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  22. Axial Slot Casing Treatment To Improve The Stall Margin Under Circumferential Total Pressure Distortion On An Axial Flow Compressor Juan Du*, YiHan Li, Wenqiang Zhang, Jichao Li, Hongwu Zhang (2022), DOI: 10.33737/gpps21-tc-260,

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  23. Effect Of Circumferential Total Pressure Distortion On Stability In An Axial Flow Compressor Yang Liu, Jichao Li, Juan Du, Hongwu Zhang, Chaoqun Nie (2022), DOI: 10.33737/gpps21-tc-279,

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  24. Effects of Inlet Guide Vane Variability on Aerodynamic Performance of a 1.5-Stage Transonic Axial Compressor Guanghui REN, Shaojuan GENG, Hongwu ZHANG, Xiaofang WANG, Jinguang YANG (2022), DOI: 10.33737/gpps21-tc-283,

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  25. Experimental Investigation Of Circumferential Inlet Distortion On Partial Surge Type Stall Inception In A Transonic Axial Compressor Jiandong Yan, Wenqian Wu, Tianyu Pan, Qiushi Li (2022), DOI: 10.33737/gpps21-tc-287,

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  26. A Review Of The Analytical And Numerical Methods For Axial Compressor Surge Juan Du*, Hongliang Zhao, Hongwu Zhang, Wenqiang Zhang, Chaoqun Nie (2022), DOI: 10.33737/gpps21-tc-296,

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  27. Post-stall behavior of 2-stage compressor Ziwei Wang, Bin Li, Junbin Liu, Jingfan Chen, Yao Liu (2022), DOI: 10.33737/gpps21-tc-300,

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  28. Influence Of Fan Rotor Leading Edge Erosion On The Flow Characteristics Of The Compression System Chenlei Huang, Lei Shi, Wenbo Wu, Peng Yu, Long Ma, Qi Jiang (2022), DOI: 10.33737/gpps21-tc-319,

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  29. Propeller Design and Performance Evaluation with Partially Prescribed Velocity Distribution Sebastian Lück, Jan Göing, Tim Wittmann, Bastian Kirsch, Leroy Benjamin, Jens Friedrichs (2022), DOI: 10.33737/gpps21-tc-328,

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  30. Sensitivity of Compressor Performance and Tip-Leakage Vortices to Inhomogeneous Casing Heat-Flux Distributions Dajan Mimic*, Philipp Sauer, Joerg R. Seume (2022), DOI: 10.33737/gpps21-tc-337,

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  31. Effect of Blade Loading Distribution on Flow Stability of Axial Compressor Dakun Sun*, Dengke Xu, Xu Dong, Xiaofeng Sun (2022), DOI: 10.33737/gpps21-tc-364,

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  32. Study of Low-Speed Modelling Method on Corner Separation Control Using Blade End Slots in a Highly Loaded Compressor Cascade Yumeng Tang*, Yangwei Liu*, Yantong Zhang (2022), DOI: 10.33737/gpps21-tc-336,

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  1. Impact of different diffusion models on NO production in NH3/H2/air turbulent flames using DNS Cheng Chi, Dominique Thévenin (2022), DOI: 10.33737/gpps21-tc-3,

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  2. Numerical Simulation of Primary Atomization of Swirling Liquid Sheet Using Transforming Algorithm Xiaoqiang Sun, Hong Yan, Fuzhen Chen (2022), DOI: 10.33737/gpps21-tc-58,

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  3. Study of Atomization Model of Prefilming Atomizer Considering Mass and Heat Transfer Processes Hong Yan*, Jingyun Zhao, Fuzhen Chen (2022), DOI: 10.33737/gpps21-tc-84,

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  4. Numerical simulation analysis on flow characteristics and kerosene distribution characteristics of a cavity flame holder with preheating evaporation chamber Wen-bo Yu, Yu-xin Fan, Chen Yue (2022), DOI: 10.33737/gpps21-tc-86,

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  5. Investigation on the performance improvement of an outer ring application on triple swirler combustor Da Mo, Junfeng Zhang, Yixiong Liu, Ming Cheng, Chengkai Zhang, Bin Wan (2022), DOI: 10.33737/gpps21-tc-114,

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  6. Singular Spectrum Analysis Of Transient Heat Release In A Premixed Swirl Combustor Yang Yang, Zhijian Yu (2022), DOI: 10.33737/gpps21-tc-135,

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  7. Effects of Wall Confinement on the Flame Topology and Lean Blowout Characteristics in a Partially Premixed Single Swirl Gas Turbine Model Combustor Yuyang Li*, Dmitriy Markovich, Leonid Chikishev, Vladimir Dulin, Tianyou Lian, Xiaoyuan Yang, Zhongya Xi, Zundi Liu, Xiaoxiang Shi (2022), DOI: 10.33737/gpps21-tc-137,

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  8. Experimental and Numerical Investigation of Jet Velocity Effects on Parallel Jet Combustor Characteristics of Hydrogen Enriched Fuel Zhigang Liu, Yan Xiong, Zhedian Zhang (2022), DOI: 10.33737/gpps21-tc-146,

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  9. Predicting the Ignition Sequences in a Separated Stratified Swirling Spray Flame with Stochastic Flame Particle Tracking Qing Xie, Chi Zhang, Siheng Yang, Hao Cheng, Zhuyin Ren (2022), DOI: 10.33737/gpps21-tc-156,

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  10. Effects of Inlet Air Temperature and Steam Addition on the Realization of MILD Combustion for Humid Air Turbine Ziru Zhu, Yan Xiong, Zhedian Zhang (2022), DOI: 10.33737/gpps21-tc-162,

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  11. Mode Shape and Eigenfrequency Analysis based on Helmholtz Equation for Thermo-acoustic Combustion Instability Juan Wu, Yinli Xiao, Yipin Lu, Zhuoqiang Chen, Wang Sen (2022), DOI: 10.33737/gpps21-tc-200,

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  12. Hybrid Eulerian-Lagrangian simulations of liquid jet atomization in swirling cross flow Tai Jin, Gaofeng Wang, Kun Luo, Jianren Fan (2022), DOI: 10.33737/gpps21-tc-250,

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  13. The Effects of Strong-Weak Swirling Interaction on Emissions In a Multi- Nozzle Model Combustor Bing Ge*, Ming Jin, Ting Shi, YuDi Lu, ShuSheng Zang (2022), DOI: 10.33737/gpps21-tc-251,

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  14. Assessment of Finite Rate Chemistry Combustion Models in a Turbulent Dilute Ethanol Spray Flame Yu Yin, Tianwei Yang, Hua Zhou, Zhuyin Ren (2022), DOI: 10.33737/gpps21-tc-252,

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  15. Single-Shot Spontaneous Raman Scattering Measurements In A Reverse-Flow Aeroengine Model Combustor Under Elevated Inlet Temperature And Pressure Shuzhen Chen, Beichen Lin, Li Shen, Jianghuai Cai, Yancheng You, Wenjiang Xu (2022), DOI: 10.33737/gpps21-tc-270,

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  16. Assessment of Adaptive chemistry via prepartitioning of composition space and mechanism reduction for the Simulation of MILD Combustion Pietro Pagani, Francesco Contino, Alessandro Parente (2022), DOI: 10.33737/gpps21-tc-285,

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  17. Investigation On The Lean Blow-Out Characteristics In Concentric Staged Combustor Hongxia Liang, Longyue Wang, Jianqin Suo (2022), DOI: 10.33737/gpps21-tc-302,

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  18. Effects of Scaling Laws on Flow and Combustion Characteristics of Lean Premixed Swirl Burners Xie Wenda, Ge Bing, Shi Ting, Zang Shusheng (2022), DOI: 10.33737/gpps21-tc-343,

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  19. Investigations On The Effects Of Flue Gas Recirculation On The Combustion Instability Of A Premixed Flame For The Low Nox Emissions Deng Pan, Tong Zhu, Chenzhen Ji (2022), DOI: 10.33737/gpps21-tc-347,

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  20. Analysis Of Combustion Instability Modes For A Partially Premixed Swirl Combustor By Flame Transfer Function With The Three-Dimensional Thermoacoustic Model Enlei Ke, Ziyu Wang, Jiaying Cheng, Deng Pan, Tong Zhu, Chenzhen Ji (2022), DOI: 10.33737/gpps21-tc-348,

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  21. Automatic extraction of Chemical Reactor Networks from CFD data via advanced clustering algorithms Matteo Savarese, Alberto Cuoci, Ward De Paepe, Alessandro Parente (2022), DOI: 10.33737/gpps21-tc-349,

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  22. Feeding H2 Admixtures In A Micro-Gas Turbine: A CFD Study Lorenzo Giuntini, Chiara Galletti, Alessandro Parente (2022), DOI: 10.33737/gpps21-tc-356,

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  1. Design and performance analysis of centrifugal compressor for supercritical carbon dioxide Brayton cycle Feng Zhang*, Gaoliang Liao, Qihan Zhang (2022), DOI: 10.33737/gpps21-tc-14,

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  2. Aerodynamic optimization for the vaned diffusers of an ultra-high-pressure-ratio centrifugal compressor based on an efficient machine learning algorithm Li Qingkuo, Zhang Ziqing (2022), DOI: 10.33737/gpps21-tc-31,

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  3. Numerical Investigations on Slip Characteristics and Slip Onset Position in High-Loaded Backswept Centrifugal Impellers Chaowei Zhang, Xuezhi Dong, Xiyang Liu, Hualiang Zhang (2022), DOI: 10.33737/gpps21-tc-87,

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  4. Effects of impeller blades with bow trailing edge on centrifugal compressor performance ZiLiang LI, XinGen LU, Ge Han, Junqiang Zhu (2022), DOI: 10.33737/gpps21-tc-96,

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  5. Evolution of unsteady vortex structures and rotating stall cells in a centrifugal compressor with vaneless diffuser Siya Jiang, Cheng Tian, Song Fu (2022), DOI: 10.33737/gpps21-tc-152,

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  6. A study of real gas effect on SCO2 compressor performance using similarity method Pengcheng Xu, Zhengping Zou (2022), DOI: 10.33737/gpps21-tc-154,

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  7. Investigation of a Highly Loaded Transonic Centrifugal Compressor Using an Advanced Design Method Ziliang Li *, Luwen Feng, Yapeng Xue, Yanhui Wu (2022), DOI: 10.33737/gpps21-tc-172,

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  1. Hybrid location-allocation algorithm for large scale energy system planning: A case study of the hydrogen supply chain in Belgium Davide Tonelli, Alessandro Parente, Francesco Contino (2022), DOI: 10.33737/gpps21-tc-37,

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  2. Range of application for a self-sufficient energy system with hydrogen as energy carrier in remote areas Tin Jurisic, Sebastian Rehfeldt, Michel Kneller, Harald Klein (2022), DOI: 10.33737/gpps21-tc-209,

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  1. Research on the Aero Design System for the Ultra-Highly-Loaded Aspirated Fan Lei Wang, Bo Liu (2022), DOI: 10.33737/gpps21-tc-57,

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  2. Effect of axial slot casing treatment on a counter-rotating axial compressor performance and stability Yanchao GUO, Limin GAO, Lei WANG, Xiaochen MAO (2022), DOI: 10.33737/gpps21-tc-133,

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  3. Large Eddy Simulation Of Corner Stall Control In A Linear Compressor Cascade By Blended Blade And Endwall Technique Huiling Zhu, Ling Zhou, Jiabin Li, Tongtong Meng, Lucheng Ji (2022), DOI: 10.33737/gpps21-tc-188,

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  4. Experimental validation of a corner stall control methodology using parametrised guide fins Gabriel Mondin, William Riéra, Pierre Duquesne, Xavier Ottavy (2022), DOI: 10.33737/gpps21-tc-308,

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  1. Experimental study on the uncertainties of individual blade vibrational parameter estimation based on blade tip timing Zhicheng Xiao, Yiming Meng, Jianping Li, Chengwei Fan, Hua Ouyang (2022), DOI: 10.33737/gpps21-tc-73,

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  2. Application of particle streak velocimetry based on binocular vision in cascade flow channel Mingjun Feng, Wu Zhou, Fangting Wang (2022), DOI: 10.33737/gpps21-tc-122,

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  3. Numerical Investigation of the Reynolds Number Effect on Five-Hole Probe Calibration Weihan Fan, Wenbo Xie, Hongmei Jiang, Shaopeng Lu, Yuze Zhang, Qiang Zhang (2022), DOI: 10.33737/gpps21-tc-148,

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  4. Geometric measurement of film-cooling holes using co-axial light-field imaging Shengming Xu, Fei Zeng, Shengxian Shi (2022), DOI: 10.33737/gpps21-tc-160,

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  5. Noise Of Future Aircraft Propulsion: Sources And Design Considerations Georgios Protopapadakis, Vasilis Gkoutzamanis, Stavros Vouros, Konstantinos Kyprianidis, Anestis I. Kalfas (2022), DOI: 10.33737/gpps21-tc-310,

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  6. 1D Analytic and Numerical Analysis of Multilayer Laminates and Thin Film Heat Transfer Gauges Mark Baker, Budimir Rosic (2022), DOI: 10.33737/gpps21-tc-346,

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  1. Experimental study on vortex sound interaction of acoustic resonance and its suppression in a flow duct Yilei Fu, Jiaqi Zhang, Zhiliang Hong, Mingsui Yang (2022), DOI: 10.33737/gpps21-tc-118,

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  2. Influence Of Uneven Blade Tip Clearances On Aeroacoustic Characteristics Of Centrifugal Compressors Mingxu Qi*, Meijie Zhang, Hong Zhang (2022), DOI: 10.33737/gpps21-tc-144,

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  3. Influence of Uneven Blade Tip Clearances on Aeroacoustic Characteristics of Centrifugal Compressors Weidong Shao, Bo Huang, Xinwen Zhang, Changchun Liu, Bing Lin (2022), DOI: 10.33737/gpps21-tc-195,

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  4. Research on Aerodynamics and Aeroacoustics of Duct Fan based on Panel-Vortex Particle Method Qian Liu, Hanru Liu, Haitong Wang, Jiahui Li, Yangang Wang (2022), DOI: 10.33737/gpps21-tc-254,

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  1. Parameter Selection For Aeroengine Transient State Gas Path Analysis Kun Yang, Qiuye Tu, Yunhao Zeng, Jing Xuan (2022), DOI: 10.33737/gpps21-tc-36,

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  2. Aeroengine Multi-Fault Diagnosis Based on Hierarchical Multi-mode Filtering Hao Jiang, Xinyu Ren, Xiaojian Fang (2022), DOI: 10.33737/gpps21-tc-136,

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  3. Localization Of Breathing Cracks In Engineering Structures With Transmissibility Function-Based Features Quankun Li, Zihao Li, Mingfu Liao, Kang Zhang (2022), DOI: 10.33737/gpps21-tc-183,

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  4. Data Science-Based Trend Analysis In Research And Development Of Turbomachinery Mark Ziesse, Joerg R. Seume (2022), DOI: 10.33737/gpps21-tc-286,

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  5. Research progress of aero-engine gas-path fault diagnosis technology based on machine learning Guo Yanqiang, Sun Zhensheng, Hu Yu, Zhang Yin, Wangjiangbin (2022), DOI: 10.33737/gpps21-tc-326,

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  1. Effect of Fan Blade Vibration Mode on Flutter Stability Xinkai Jia, Huang Huang, Dingxi Wang (2022), DOI: 10.33737/gpps21-tc-182,

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  2. Flutter Analysis Of Blisks With Friction Ring Dampers Yekai Sun, Jie Yuana, Loic Salles (2022), DOI: 10.33737/gpps21-tc-42,

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  3. Multi Traveling Wave Flutter Onset In Tuned Bladed-Disks Javier Gonz lez-Monge, Salvador Rodr guez-Blanco, Carlos Martel (2022), DOI: 10.33737/gpps21-tc-28,

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  4. Structural Optimization Of The Wing Box For A Hybrid-Electric Commuter Aircraft Christos P. Nasoulis, Panagiotis Tsirikoglou, Anestis I. Kalfas (2022), DOI: 10.33737/gpps21-tc-211,

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  5. Study on Structural Strength and Air-tightness Analysis of a Large Axial Compressor Casing Zhang Xiaolong, Li Bing, Yuan Zhicai, Shen Zhen, Zhang Wushuai, Xu Jing, Zhao Peng, Chen Guang (2022), DOI: 10.33737/gpps21-tc-229,

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  6. Parametric Analysis Of The Shear Lag Effect In Serpentine Nozzles Under Fluid-Thermal-Solid Coupling Influence Sheng Huang, Le Rong (2022), DOI: 10.33737/gpps21-tc-233,

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  7. Investigation Of Lock-In Phenomenon Of A Fle Fan Yun Zheng, Qingzhe Gao, Hui Yang, Da Lei (2022), DOI: 10.33737/gpps21-tc-273,

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  8. Analysis Of Structurally And Aerodynamically Mistuned Oscillating Bladerow Using Fully-Coupled Method H. M. Phan, L. He (2022), DOI: 10.33737/gpps21-tc-330,

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  9. Influence Of Axial Gaps On Forced Response Of Different Mode Shapes In A Low-Pressure Compressor Hye Rim Kim*, Dajan Mimic, Joerg R. Seume (2022), DOI: 10.33737/gpps21-tc-338,

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  10. Nonlinear Flutter Analysis Of The Zero Nodal Diameter Of A Labyrinth Seal Roque *, Michele Greco, J. Luis Matabuena (2022), DOI: 10.33737/gpps21-tc-354,

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  11. High fidelity finite element model updating and deviation characterization method for geometric mistuned bladed disks Daosen Liang, Rui Zhang, Yulin Wu, Zichu Jia, Zhifu Cao, Jianyao Yao (2022), DOI: 10.33737/gpps21-tc-360,

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  1. LES-Based Analysis of Unsteadiness and Instability of Tip leakage Vortex in Turbine Rotor Zuojun WEI*, Ming NI, Guangming REN*, Lei ZHAO (2022), DOI: 10.33737/gpps21-tc-21,

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  2. Les Prediction Of Transitional Flows In LP Turbine Cascades: Flow Phenomena And Effects Of Numerical Setup Atsushi Tateishi, Naoki Tani, Yasuhiro Okamura, Masaaki Hamabe (2022), DOI: 10.33737/gpps21-tc-61,

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  3. Study on dynamic characteristics of a combined air pressure reducing valve CAI Bing, Liu Yuhu, Cheng Xiaofeng (2022), DOI: 10.33737/gpps21-tc-305,

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  4. Non-Intrusive Flow distortion measurements within a Turbofan Intake (NIFTI)- De-risking the test campaigns with CFD analysis W. Zhang, B. Tiedemann, S. Hegen, M. Vahdati, Pavlos Zachos, F. Zhao (2022), DOI: 10.33737/gpps21-tc-316,

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  5. Study on Unsteady Flow Characteristic in a Transonic Axial Compressor Rotor at Near Stall Condition Ziyun Zhang, Yanhui Wu, Zhidong Chi (2022), DOI: 10.33737/gpps21-tc-321,

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  6. From Measurement To Simulation A Review Of Aerodynamic Investigations Of Real Rough Surfaces By DNS Sebastian Kurth, Kenan Cengiz, Lars Wein, Joerg R. Seume (2022), DOI: 10.33737/gpps21-tc-213,

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  1. Efficient Analysis of Unsteady Flows Within Multi-Stage Turbomachines Using the Coupled Time and Passage Spectral Method Ding Xi Wang, Sen Zhang, Xiuquan Huang (2022), DOI: 10.33737/gpps21-tc-4,

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  2. Development of Aspirated Ultra-Short Intakes for Aerodynamic Off-Design Analysis Lennart Harjes, Legin Benjamin, Jonas Grubert, Constance Heykena, Jens Friedrichs (2022), DOI: 10.33737/gpps21-tc-23,

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  3. Forced response analysis of the rotor blade rows with the ROM-based aeroelastic model Jingyuan Yang, Weiwei Zhang (2022), DOI: 10.33737/gpps21-tc-25,

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  4. Numerical Dissipation Effects on Detached Eddy Simulation of Turbomachinery Flows Cheng Tian, Siya Jiang, Song Fu (2022), DOI: 10.33737/gpps21-tc-74,

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  5. Whole Engine Thermal Analysis For Calculation Of Clearances In A Heavy-Duty Gas Turbine Hossein Shakeri, Mohsen Shokrollahi, Amir Poursamad (2022), DOI: 10.33737/gpps21-tc-88,

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  6. A three-dimensional freeform blading tool based on NURBS curves and surfaces implemented in Python Weihua Li, Shenren Xu (2022), DOI: 10.33737/gpps21-tc-91,

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  7. Study on the Flow Characteristics of Fan Coupled Nacelle Intake under Different Angle of Attack Min Qi, Zhanxue Wang, Li Zhou, Wenjian Deng (2022), DOI: 10.33737/gpps21-tc-109,

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  8. Research On Aero Engine Intake Distortion Based On 3D CFD Full Engine Simulation Yibing Xu, Wantong Wu, Wei Liu, Ying Piao (2022), DOI: 10.33737/gpps21-tc-117,

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  9. Investigation of a WallDistanceFree Spalart–Allmaras Turbulence Model for Turbomachinery Applications Junjie Yin, Dingxi Wang (2022), DOI: 10.33737/gpps21-tc-193,

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  10. Immersed Boundary Method For The Investigation Of Real Surfaces With Isotropic And Anisotropic Roughness Components Jan Dominik Ahrens, Sebastian Kurth, Kenan Cengiz, Lars Wein, Joerg R. Seume (2022), DOI: 10.33737/gpps21-tc-214,

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  11. Machine Learning Based Design Optimization of Centrifugal Impellers Ao Zhang, Yan Liu, Jinguang Yang, Zhi Li, Chuang Zhang, Yiwen Li (2022), DOI: 10.33737/gpps21-tc-235,

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  12. Effects of Different CO2 equations of state on Condensation Position in Numerical Investigation Lei Zhang, Zhenyu Yang, Zheng Dong, Qian Zhang, Enhui Sun (2022), DOI: 10.33737/gpps21-tc-247,

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  13. Influence of shield on supersonic inlet characteristics Feichao Cai, Xing Huang (2022), DOI: 10.33737/gpps21-tc-299,

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  14. Influence of shield on supersonic inlet characteristics Feichao Cai, Xing Huang (2022), DOI: 10.33737/gpps21-tc-299,

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  15. Compressor Tandem Cascade Flow Prediction by Adaptive POD-RBFN Reduced Order Model Xun Shang, Hanru Liu*, Yican Du, Zhijie Hu (2022), DOI: 10.33737/gpps21-tc-313,

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  16. Evaluation Of Ddes Based On SST K-ω Model With Different Shielding Functions For Tip Leakage Flow In Turbomachinery Yangwei Liu*, Yanfei Gao, Guangyu Wang, Yumeng Tang (2022), DOI: 10.33737/gpps21-tc-320,

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  17. Assessment of Rans and SBES Methods for the Prediction of Corner Separation in Axial Flow Compressors Wei Sun (2022), DOI: 10.33737/gpps21-tc-341,

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  18. Unsteady Analysis with Throughflow Concept Yinbo Mao, Xinrong Su, Xin Yuan (2022), DOI: 10.33737/gpps21-tc-345,

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  1. Surrogate-Based Aerodynamic Shape Optimization Of Contra Rotating Open Rotor Qihang Wang, Li Zhou, Zhanxue Wang (2022), DOI: 10.33737/gpps21-tc-76,

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  2. Multi-objective Optimization of A Three-shaft High Bypass Ratio Engine for EIS2050 Yixiong Liu*, Devaiah Nalianda, Da Mo, Wei Wang, Yunwu Wu, Qing Du (2022), DOI: 10.33737/gpps21-tc-113,

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  3. Sequential ensemble multi-objective optimization algorithm and its application on the multi-working performance optimization of the variable cycle engine Yifan Ye, Zhanxue Wang, Xiaobo Zhang (2022), DOI: 10.33737/gpps21-tc-145,

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  4. Generative Transfer Optimization for Aerodynamic Design Zhendong Guo, Wei Sun, Liming Song, Jun Li, Zhenping Feng (2022), DOI: 10.33737/gpps21-tc-225,

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  5. Research On Applying Free-Form Deformation In Airfoil Parameterization And Aerodynamic Optimization Handuo Hu, Yanping Song, Jianyang Yu, Yao Liu, Fu Chen (2022), DOI: 10.33737/gpps21-tc-241,

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  6. Aerodynamic Rotor Blade Design For Small Wind Turbines With Focus On Turbulent Inflow Conditions Matthias Schmid, Joerg R. Seume (2022), DOI: 10.33737/gpps21-tc-332,

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  1. Quantification of Compressor Aerodynamic Performance Deviation due to Manufacturing Uncertainty Using the Adjoint Method Qian Zhang, Shenren Xu, Xianjun Yu, Jiaxin Liu, Dingxi Wang, Xiuquan Huang (2022), DOI: 10.33737/gpps21-tc-59,

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  2. Effects Of Geometric And Operational Uncertainties On The Aerodynamic Performance Of A Centrifugal Compressor Stage Rui Zhu, Yaping Ju, Chuhua Zhang (2022), DOI: 10.33737/gpps21-tc-159,

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  3. Performance Impact of Uncertain Variations of Inlet Flow for Axial Compressor Blades Zeshuai Chen, Jiaqi Luo, Yalu Zhu, Zhiheng Xia (2022), DOI: 10.33737/gpps21-tc-168,

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  1. Improving the Film Cooling by Controlling the Vortex Structures Chao Zhou*, Mostafa Moosania, Qiuyin Wang (2022), DOI: 10.33737/gpps21-tc-19,

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  2. Numerical study on flow and heat transfer characteristics in an impingement/effusion cooling system with high blockage ribs Dehai Kong, Zhenyuan Ma, Sergey A. Isaev, Cunliang Liu (2022), DOI: 10.33737/gpps21-tc-44,

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  3. Large Eddy Simulation of Transonic Film Cooling with Injection Through Cylindrical Orifices Including Shockflow Interaction Hao Guo, Peixue Jiang, Yinhai Zhu* (2022), DOI: 10.33737/gpps21-tc-45,

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  4. Numerical analysis on system performance of a pre-swirl air supply system about the improvement of receiver hole structure Wenbin Gong, Gaowen Liu, Aqiang Lin, Fei Wang, Zhiwu Wang (2022), DOI: 10.33737/gpps21-tc-65,

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  5. Numerical Investigations into the Effects of Turning Vanes on Heat Transfer and Flow of a 2-Pass Ribbed Internal Cooling Channel with a UShape Bend Jiang LEI *, Jiaxu YAO, Ruishan LU, Pengfei SU, Yu FANG (2022), DOI: 10.33737/gpps21-tc-83,

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  6. Calculation Model of Rotating Orifices Discharge Coefficient Considering the Influence of Internal and External Crossflows Jie Wang, Tian Qiu (2022), DOI: 10.33737/gpps21-tc-110,

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  7. A Temperature-Gradient Correction Method for Film Cooling Effectiveness Measurement using Endoscope-Based PSP Technique Kechen Wang, Di Peng, Yingzheng Liu, Wenwu Zhou* (2022), DOI: 10.33737/gpps21-tc-132,

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  8. Simultaneous Measurements of Velocity and Concentration Fields in An Inclined Jet in Crossflow Xu Zhang, Shengwei Zhao, Chuangxin He, Yingzheng Liu, Wenwu Zhou (2022), DOI: 10.33737/gpps21-tc-158,

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  9. Numerical Simulation on Internal Flow and Heat Transfer of Sweeping Jet and Film Composite Cooling on a Flat Plate Xiangcan Kong, Ziqing Zhang, Guoqing Li, Yanfeng Zhang (2022), DOI: 10.33737/gpps21-tc-164,

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  10. Large-eddy simulation of shaped hole film cooling with the influence of streamwise pressure gradient Kexin Hu, Qingsong Wang, Xinrong Su, Xin Yuan (2022), DOI: 10.33737/gpps21-tc-165,

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  11. fects of High Buoyancy Parameter on Flow and Heat Transfer of Two-Pass Smooth Channels Wenbin He, Ruishan Lu, Jiaxu Yao, Ke Zhang, Junmei Wu, Jiang Lei* (2022), DOI: 10.33737/gpps21-tc-174,

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  12. The experimental study on the film cooling in the convergent-divergent nozzle with PSP technique Feng Liu, Cun-liang Liu, Zhao Ma, Tao Guo (2022), DOI: 10.33737/gpps21-tc-199,

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  13. PIV Measurements of Turbulent Flows Along the Ribbed Square Duct Under Rotational Condition Jincheng Shi, Haiwang Li, Ruquan You (2022), DOI: 10.33737/gpps21-tc-203,

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  14. The Effect of Impingement-Effusion Cooling Structure on Adiabatic Film Effectiveness Shanyou Wang, Xueying Li, Jing Ren (2022), DOI: 10.33737/gpps21-tc-221,

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  15. Effects of streamwise vortices on the film cooling effectiveness of a fanshaped hole Xiao-feng Cui, Dai Ren, Peng-min Liu, Chi-xiang Lin (2022), DOI: 10.33737/gpps21-tc-228,

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  16. Effects of Local Blockage on Film Cooling Effectiveness of a Fan-Shaped Hole Fed by Crossflow Pengmin L, Xiaofeng C, Chixiang L, Ren D (2022), DOI: 10.33737/gpps21-tc-231,

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  17. Generative Design of Internal Cooling Channels for Gas Turbine Blades Li Yang*, Binyan Wang, Zijie Lu, Bocheng Yu, Xinxing Wang, Weihong Li (2022), DOI: 10.33737/gpps21-tc-256,

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  18. Numerical Investigation of Different Turbulence Models Applied in Combined Impingement and Film Cooling Min Yao, Jieli Wei, Zhuyin Ren, Xiaohua Gan (2022), DOI: 10.33737/gpps21-tc-265,

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  19. Research status and development trend of rotating internal cooling of a gas turbine blade Xinxin Guo, Xueying Li, Jing Ren (2022), DOI: 10.33737/gpps21-tc-284,

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  20. Experimental Study on Overall Cooling Effectiveness of Three-layer Laminate for Stealth Aircraft Tail Boom Feifei Cao, Zhao Ma, Cun Liang Liu, Chao Dong, Tian Liang Zhou (2022), DOI: 10.33737/gpps21-tc-293,

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  21. Effects of hole arrangement and trenched hole on multirow film cooling Wen Wang, Jiahuan Cui, Shaoxing Qu (2022), DOI: 10.33737/gpps21-tc-303,

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  22. Conjugate Flow and Heat Transfer Mechanism between the Rib Cooling and Film Cooling Wei Jin, Shaoen Peng, Junmei Wu, Jiang Lei, Wentao Ji (2022), DOI: 10.33737/gpps21-tc-352,

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  23. Effects of the Ceramic Matrix Composites with Anisotropic Thermal Conductivities on the Endwall Film Cooling with Laid-Back Shaped Hole Kun Du, Qihao Chen, Xianlong Meng, Tingrui Liang, Cunliang Liu (2022), DOI: 10.33737/gpps21-tc-357,

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  24. Experimental Study of Time-Resolved Film Cooling Effectiveness of Compound-Angled Fan-Shaped Film-Hole at Curved Wall Tiao Zhang, Jian Pu, Jian-hua Wang (2022), DOI: 10.33737/gpps21-tc-257,

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  1. Quantification of Swirl Distortions Caused by S-shape Inlet Ducts Zhenyu LI, Xu DONG, Dakun SUN, Xiaofeng SUN (2022), DOI: 10.33737/gpps21-tc-38,

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  2. Effectiveness of Active Flow Control Techniques in an Advanced S-Shaped Engine Intake Philipp Max, Marcel Stoessel, Michael Krummenauer, Reinhard Niehuis (2022), DOI: 10.33737/gpps21-tc-102,

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  3. Numerical investigation of an aggressive s-shaped compressor transition duct with combined boundary layer suction Song Huang, Chengwu Yang, Shengfeng Zhao, Han Ge, Hongzhi Cheng, Xingen Lu (2022), DOI: 10.33737/gpps21-tc-170,

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  1. A 2D Axisymmetric Approach for Low Pressure Turbine Tip Sealing Design Zhuqing YI, Yuan JIN, Wenqi XU, Olivier JUNG (2022), DOI: 10.33737/gpps21-tc-68,

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  2. The Effect of the Front Plate with Ribs on Brush Seal Flow Characteristics Yuxin Liu*, Benzhuang Yue, Xiaozhi Kong, Hua Chen, Huawei Lu (2022), DOI: 10.33737/gpps21-tc-104,

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  3. Analysis of Wheel Space Ingress in a One-Stage Axial Turbine Thomas Hoesgen, Matthias H. Meinke, Wolfgang Schr der (2022), DOI: 10.33737/gpps21-tc-192,

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  4. Investigation of Staggered Labyrinth Tip Shroud on Flow Mechanism of Low-Pressure Turbine Wei Tan, Ziqing Zhang, Xiao Qu, Lin Li, Yanfeng Zhang (2022), DOI: 10.33737/gpps21-tc-325,

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  5. Influence of Honeycomb Structures on Labyrinth Seal Aerodynamics Marcel Oettinger, Tim Kluge, Joerg R. Seume (2022), DOI: 10.33737/gpps21-tc-339,

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  1. Research on Optimal Design of Gas Turbine Blade Tip Cooling Lei HE, Yueru LI, Jinjie ZHAO, Lianhui ZHAO, Xiaocheng ZHU, Chaohui DU (2022), DOI: 10.33737/gpps21-tc-5,

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  2. An investigation on AerofoilShaped Blade Profiles for Centrifugal Turbines Yu Min Liu, Patrick Hendrick, ZhengPing Zou, Frank Buysschaert (2022), DOI: 10.33737/gpps21-tc-7,

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  3. Turbomachinery Analysis and Design Using BodyForce Modeling in SU2 Evert C Bunschoten, Nitish Anand, Matteo Pini (2022), DOI: 10.33737/gpps21-tc-13,

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  4. Effect of Leading-Edge/Trailing-Edge Geometry on Uncertainty Aerodynamic Performance of a 2D Low-pressure Turbine Blade Xiaojing Wang, Zhengping Zou (2022), DOI: 10.33737/gpps21-tc-18,

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  5. Aerodynamic and Strength Improvement of the Axial Turbine of a Helicopter GTE G.М. Popov, Evgenii S. Goriachkin, Oleg V. Baturin, A.I. Korneeva, Igor Egorov (2022), DOI: 10.33737/gpps21-tc-34,

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  6. Calculating the Parameters of a Gas Turbine Engine Taking into Account the Uncertainty of the Initial Data Oleg V. Baturin, Pau Nicolalde, Grigorii M. Popov, Valery N. Matveev, Yulia D. Novikova (2022), DOI: 10.33737/gpps21-tc-35,

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  7. A Numerical Study of Influence of Internal Crack on Thermal Property of APS-TBCs Yun Long, Yuzhang Wang, Xiaohu Chen, Kanru Cheng, Licheng Shi, Runxuan Sang (2022), DOI: 10.33737/gpps21-tc-54,

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  8. Effects of Partial Suction Side Rim on the Aerodynamics and Heat Transfer Cooling Performance of the Turbine Blade Squealer Tip Chengtian XU, Zhigang LI, Jun LI*, Liming SONG (2022), DOI: 10.33737/gpps21-tc-63,

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  9. An Aerodynamic Performance Optimization Method Applied to the Intake Grille of Active Clearance Control System Shuyi Zhang, Bo Yang, Hong Xie, Guoming Zhu, Moru Song (2022), DOI: 10.33737/gpps21-tc-64,

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  10. Investigation of Water Droplet Erosion in The Radial Turbine of a Fuel Cell Turbocharger Tim Wittmann, Sebastian Lück, Christoph Bode, Jens Friedrichs (2022), DOI: 10.33737/gpps21-tc-72,

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  11. Effects of Surface Roughness on Flow Losses of a High-Loading Low-Pressure Turbine Cascade Xian Zeng, Jiaqi Luo (2022), DOI: 10.33737/gpps21-tc-75,

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  12. Experiment investigation on flow characteristics in a high speed rotor-stator cavity with axial air inflow Ran Chang, Gaowen Liu, TianHeng Zha, Qing Feng (2022), DOI: 10.33737/gpps21-tc-101,

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  13. A Fluid-Thermal Analysis of Partial Admission Axial Turbines Hanwei Wang, Kai Luo, Qiushi Yang, Chuang Huang, Kan Qin (2022), DOI: 10.33737/gpps21-tc-105,

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  14. Optimum cooling performance of a multiple-jets impingement cooling system by controlling the inlet flow condition Long Meng, Haiwang Li, Xie Gang, Zhiyu Zhou* (2022), DOI: 10.33737/gpps21-tc-112,

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  15. Influence of Combustor Exit Conditions on Cooling Performance of NGV Endwall with Double Row Cooling Holes Zhenping Feng*, Ruocheng Li, Wenhao Zhang, Zhiduo Wang (2022), DOI: 10.33737/gpps21-tc-116,

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  16. Boundary layer separation control of low-pressure turbine blades based on oscillating jet Luanliang Zhou, Zifeng Jing, Xin Wen, Yingzheng Liu (2022), DOI: 10.33737/gpps21-tc-124,

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  17. Aerodynamic design and performance analysis of the ultra-high expansion ratio turbine for trans-media engines Jie Gao*, Siyu Wu, Cheng Zhou, Weliang Fu (2022), DOI: 10.33737/gpps21-tc-125,

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  18. URANS Simulations of Deposition in a Rotor Passage of the First-Stage Turbine for an Aero-Engine Zhenping Feng*, Zihan Hao, Xing Yang, Xiangyu Wang (2022), DOI: 10.33737/gpps21-tc-130,

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  19. The Influence of Back Pressure Change on the Leakage Flow Characteristics of the Last Stage Blade Tip Clearance of Steam Turbine Xu Han*, Yunyun Yuan, Peng Li, Zhonghe Han (2022), DOI: 10.33737/gpps21-tc-131,

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  20. Effect of Surface Tension Correction Coefficient on Non-Equilibrium Condensation Flow of Wet Steam Xu Han*, Bochuan Yao, Yunyun Yuan, Zhonghe Han (2022), DOI: 10.33737/gpps21-tc-139,

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  21. Numerical Investigations on the Unsteady Leakage Flow and Heat Transfer Characteristics of the Turbine Blade Squealer Tip Jun LI*, Shijie JIANG, Zhigang LI, Liming SONG (2022), DOI: 10.33737/gpps21-tc-153,

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  22. Effects of Anticlockwise Swirling Inflow on the Aerothermal Performance of the Turbine Vane Endwall with Film Cooling Layouts Jun LI*, Zhiyu LI, Kaiyuan ZHANG, Zhigang LI, Liming SONG (2022), DOI: 10.33737/gpps21-tc-155,

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  23. Comprehensive Calculation And Performance Analysis Of Gas Turbine Reversible Power Turbine Jie Gao*, Tianxiao Zhao, Guojie Wang, Rui Yan (2022), DOI: 10.33737/gpps21-tc-157,

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  24. Effects of Film Hole Diameter and Wall Thickness on Overall Cooling Effectiveness of Turbine Vane Leading Edge Rui Wang, Cun-liang Liu, Qi-hao Chen, Xian-long Meng (2022), DOI: 10.33737/gpps21-tc-171,

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  25. Effects of Squealer Width and Height on Aerodynamic Performance of Tip-Leakage Flow of Cavity Tips Xiaojuan He, Zhengping Zou (2022), DOI: 10.33737/gpps21-tc-175,

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  26. Influences of Depth and Rim Width of Squealer Tip on the Leakage Flow and Heat Transfer Tong Huang, Hui Li, Xinrong Su, Xin Yuan (2022), DOI: 10.33737/gpps21-tc-181,

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  27. Experimental and Numerical Investigations of Mixed Convection in Turbine Cavities for More Flexible Operations Oguzhan Murat*, Budimir Rosic, Koichi Tanimoto, Ryo Egami (2022), DOI: 10.33737/gpps21-tc-194,

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  28. Research on the Influence of Variable Geometry Power Turbine Speed Adjustable on the Overall Performance of Turboshaft Engine Zhiwei Cui, Weilin Yi (2022), DOI: 10.33737/gpps21-tc-218,

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  29. Aerodynamic Design and Analysis for a Gas Turbine Vane with Large Pitch/Chord Ratio Yongfeng Sui*, Peng Chu, Sheng Ren, Lingmin Zhou, Yao Tu (2022), DOI: 10.33737/gpps21-tc-232,

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  30. Effects of Tip Structure on the Turbine Blade Tip Phantom Cooling Performance Feng Li, Zhao Liu, Yan Shi, Zhenping Feng (2022), DOI: 10.33737/gpps21-tc-263,

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  31. Experimental Study of Turbine Blade Tip Heat Transfer with High-Speed Relative Casing Motion Wenbo Xie, Xu Peng, Hongmei Jiang, Shaopeng Lu, Yongmin Gu, Chien-Pin Chen, Qiang Zhang (2022), DOI: 10.33737/gpps21-tc-267,

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  32. Effects of Groove Structure on Aerodynamic Performance of a Turbine Blade Xin Fan, Yan Hui Wu, Xiao Bing Zhou, Xin Guo (2022), DOI: 10.33737/gpps21-tc-276,

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  33. Numerical Model of the Axial Turbine Blade Cooling Process G.М. Popov, A. A. Volkov, O. V. Baturin, V.N. Matveev, I.А. Kudryashov, A. R. Suleimanov (2022), DOI: 10.33737/gpps21-tc-277,

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  34. Effect of Free-Stream Turbulence on Endwall Flow of Highly Loaded Turbine Cascades in a Wide Range of Incidence Yin Zhao *, Wang Jiahui, Zhang Hualiang, Tang Hongtao, Xu Yujie, Chen Haisheng (2022), DOI: 10.33737/gpps21-tc-290,

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  35. Influences of Squealer Tip Geometrical Characteristics on Tip-leakage Flow in Turbine Rotor Yufan Wang, Weihao Zhang*, Zhengping Zou, Shoumin Jiang, Zhenzhe Na, Yun Chen (2022), DOI: 10.33737/gpps21-tc-175,

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  36. Method for Modeling the Thermal State of Turbine Blades of Aircraft Engines During Thermal Cycling Tests Alexander Roaldovich Lepeshkin, Zheng Guanghua (2022), DOI: 10.33737/gpps21-tc-340,

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  37. Design Optimization of the Convergent Passage Profile of a High-Load Turbine Vane Endwall Zhenping Feng*, Zhansheng Liu, Junfeng Xiao, Song Gao, Yuanyuan Li, Feilong Yu, Jingyao Duan (2022), DOI: 10.33737/gpps21-tc-292,

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  1. Thermodynamic and Thermo Economic Analysis of an Organic Rankine Cycle in a Sulfuric Acid Workshop Hanqiong Wang, Rong Xie, Jinguang Yang, Yan Liu, Donghua Zhang (2022), DOI: 10.33737/gpps21-tc-30,

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  2. A Theoretical Investigation on Thermal Insulation of Multilayer Passive Thermal Protection System With Carbon Phenolic Composites in Combustion Chamber Xianlong Zhang, Yuqing Wang, Cunliang Liu, Yujia Bao, Xiaohui Bai (2022), DOI: 10.33737/gpps21-tc-100,

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  3. The influence of working pressure on the heat transfer process and heat absorption of supercritical CO2 in thermoelectric conversion system Xuan Yang, Zhongwei Wang, Yaobin Niu, Heyang Miao (2022), DOI: 10.33737/gpps21-tc-149,

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  4. Thermal Analysis of High Speed Roller Bearing Based on Partial Power Loss Prediction Ying Pan, Wenjun Gao, Kun li (2022), DOI: 10.33737/gpps21-tc-179,

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  5. The Calculating of the Transient Temperature Field of the First Stage Segment Ring of A Gas Turbine Sui Yongfeng*, Wang Bo, Wei Jiaming, Chu Peng, Tu Yao, Chi Hongwei (2022), DOI: 10.33737/gpps21-tc-180,

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  6. Towards Real-Time Transient MGT Performance Assessment: Effective Prediction Using Accurate Component Modelling Techniques Aggelos Gaitanis, Antoine Laterre, Francesco Contino, Ward De Paepe (2022), DOI: 10.33737/gpps21-tc-215,

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  7. Investigation of Coupled Radiation-Conduction Heat Transfer in Cylindrical Systems by Discontinuous Spectral Element Method Jiazi Zhao, Yasong Sun, Yifan Li, Changhao Liu (2022), DOI: 10.33737/gpps21-tc-258,

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  8. Numerial Simulation of Turbine Blade Internal and External Heat Transfer with the Multi-Layer Coupling Method Ning Sun, Qiu-Nan Yu, Wen-Tao Ji, Ya-Ling He, Wen-Quan Tao (2022), DOI: 10.33737/gpps21-tc-309,

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  1. Transonic Comrpessor Darmstadt – Open Test Case Fabian Klausmann, Daniel Franke, Jonas Foret, Heinz-Peter Schiffer (2022), DOI: 10.33737/gpps21-tc-29,

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  2. Validation and Verification of Rans Solvers for TUDA-GLR-Openstage Transonic Axial Compressor Mingmin Zhu, Xiao He, Fabian Klausmann, Jinfang Teng, Mehdi Vahdati (2022), DOI: 10.33737/gpps21-tc-50,

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