Shaopeng Lu, Xun Liu, Songtao Wang, Xun Zhou, Guotai Feng, Zhongqi Wang (2012). Impact of Different Film-Cooling Modes at Leading Edge on the Aerodynamic and Heat Transfer Performance of Heavy Duty Gas Turbine. Asia-Pacific Power and Energy Engineering Conference (APPEEC).DOI
Feng Guo-tai (2012). Research on three-dimensional design of bowed and swept blade of transonic fan. Journal of Aerospace Power.
周逊,刘勋,王松涛,冯国泰(2011). F级地面重型燃气轮机三级涡轮和四级涡轮气动性能对比分析. Proceedings of the 2011 International Conference on Software Engineering and Multimedia Communication(SEMC 2011 V1).
刘勋,周逊,王松涛,冯国泰(2011). 端壁不同角度冷气喷射对重型燃气轮机涡轮叶栅气动性能的影响. Proceedings of the 2011 International Conference on Software Engineering and Multimedia Communication(SEMC 2011 V1).
姜斌,王松涛,冯国泰,王仲奇 (2011). Aerodynamic design of transonic fan/compressor by 3D viscous RNS combined with genetic algorithms. Journal of Harbin Institute of Technology(New series).
孙阳,姜澎,姜永艳,吴勃英,冯国泰 (2011). Application of AUSMPW scheme based on adaptive algorithm of multiwavelets in two dimensional flow field. Journal of Harbin Institute of Technology(New series).
Yang Sun, Hui Bi, Feng Guo-tai (2011). Investigation and application of high accuracy schemes in numerical simulation of turbine flow field.DOI
陈凯,黄洪雁,韩万金,冯国泰 (2010). Investigation of convection cooling guide vane with conjugate heat transfer method. Journal of Harbin Institute of Technology(New series).
温风波,王松涛,冯国泰,王仲奇(2010). 某型涡轮叶片型面匹配优化设计. 《汽轮机技术》.
Feng Guo-tai (2010). The Impact of Fuel Heat Value Change on the Flow Field in Turbine Part of 9FA Gas Turbine. Science Technology and Engineering.
Yongjun Zhang, Huishe Wang, Jianzhong Xu, Guotai Feng (2009). Study on topology and vortex structure in a diffusion cascade. Science China Technological Sciences.DOI
Ping Dong, Qiang Wang, Zhaoyuan Guo, Hongyan Huang, Guotai Feng (2009). Conjugate Calculation of Gas Turbine Vanes Cooled with Leading Edge Films. Chinese Journal of Aeronautics.DOI
Bin Hui Jiang, Songtao Wang, Guotai Feng, Zhongqi Wang (2009). Numerical Study on End-Wall Flow in Highly Loaded Supercritical Compressor Cascades.DOI
Qiang Wang, Zhaoyuan Guo, Chi Zhou, Feng Guo-tai, Wang Zhongqi (2009). Coupled Heat Transfer Simulation of a High-pressure Turbine Nozzle Guide Vane. Chinese Journal of Aeronautics.DOI
Qiang Wang, Yan Peigang, Dong Ping, Feng Guo-tai, Wang Zhongqi (2009). Application of Coolant Diffusion Equation in Numerical Simulation of Flow in Air-cooled Turbines. Chinese Journal of Aeronautics.DOI
姜澎,王强,黄洪雁,冯国泰 (2008). Numerical simulation of 3D viscous flow field of air cooled turbine blades with coolant mixing. Journal of Harbin Institute of Technology(New series).
孙阳,吴勃英,冯国泰(2008). 利用多小波自适应格式求解流体力学方程. 《力学学报》.
羌晓青,王松涛,冯国泰,王仲奇(2008). 单级低反动度轴流压气机的气动设计与分析(英文). Chinese Journal of Aeronautics.
Honglei Zhao, Songtao Wang, Han Wan-jin, Guotai Feng (2008). Aerodynamic design by jointly applying S2 flow surface calculation and modern optimization methods on multistage axial turbine. Frontiers of Energy and Power Engineering in China.DOI
Qiang Wang, Chi Zhou, Zhaoyuan Guo, Peigang Yan, Guotai Feng, Zhongqi Wang (2008). Study on Numerical Methods for Conjugate Heat Transfer Simulation of an Air Cooling Turbine. Volume 10: Heat Transfer, Fluid Flows, and Thermal Systems, Parts A, B, and C.DOI
Songtao Wang, Xiaoqing Qiang, Weichun Lin, Guotai Feng, Zhongqi Wang (2008). A Study of Parameter Selection Principle and Internal Flow Mechanism in a Multi-Stage Low-Reaction Axial Flow Compressor.DOI
Zhaoyuan Guo, Qiang Wang, Ping Dong, Chi Zhou, Guotai Feng (2008). The Key Techniques for Thermal-Flow-Elastic Coupling Numerical Simulation Platform in Turbines. Volume 10: Heat Transfer, Fluid Flows, and Thermal Systems, Parts A, B, and C.DOI
Qiang Xiaoqing, Wang Songtao, Feng Guo-tai, Wang Zhongqi (2008). Aerodynamic Design and Analysis of a Low-reaction Axial Compressor Stage. Chinese Journal of Aeronautics.DOI
Feng Guo-tai (2008). Conjugate heat transfer analysis of a high pressure turbine vane with radial internal cooling passages. Journal of Aerospace Power.
Feng Guo-tai (2008). Study on aerodynamic optimization design of multistage axial turbine under multiple working conditions. Journal of Aerospace Power.
Peng Sun, Jingjun Zhong, Guotai Feng (2007). Flow Field Analysis of Inlet Distortion in a Transonic Fan With Straight and Bowed Stator Blade.DOI
Feng Guo-tai (2007). Aerodynamic Design by Jointly Applying S2 Flow Surface Calculation and Modern Optimization Methods on Multistage Turbine. Gas Turbine Experiment and Research.
Feng Guo-tai (2007). Numerical simulation of boundary layer transition under pressure gradient. Journal of Aerospace Power.
Feng Guo-tai (2007). Analysis of flow loss induced by inlet total pressure distortion in a small fan. Journal of Aerospace Power.
Feng Guo-tai (2007). A Numerical Simulation of the Boundary Layer Transition on a Plate with Zero Pressure Gradient. Journal of Engineering for Thermal Energy and Power.
张永军,陈浮,冯国泰,苏杰先(2006). 低马赫数条件下几何折转角对平面扩压叶栅弯叶片流场性能的影响(英文). Chinese Journal of Aeronautics.
Yongjun Zhang, Fu Chen, Guotai Feng, Jiexian Su (2006). Effect of Turning Angle on Flow Field Performance of Linear Bowed Stator in Compressor at Low Mach Number. Chinese Journal of Aeronautics.DOI
Feng Guo-tai (2006). Numerical Simulation of the Influence of Bowed Blade on the Performance of Turbine Cascade with Film-Cooling. Journal of Aerospace Power.
Feng Guo-tai (2006). Numerical Simulation of the Impact of Total-pressure Distortion on the Aerodynamic Performance of Small-sized Fans. Journal of Engineering for Thermal Energy and Power.
Feng Guo-tai (2006). Numerical simulation of conjugate heat transfer in turbine blade with air cooling. Ha'erbin gongye daxue xuebao.
Mohsen Hassanvand, 王松涛, 冯国泰, 王仲奇(2004). 透平叶顶泄漏能量损失的数值计算(英文). Chinese Journal of Aeronautics.
Mohsen Hassanvand, Songtao Wang, Guotai Feng, Zhongqi Wang (2004). Calculation of the Energy Loss for Tip Leakage Flow in Turbines. Chinese Journal of Aeronautics.DOI
Hongyan Huang, Haitao Yang, Guotai Feng, Zhongqi Wang (2004). Clocking effect in a two-stage compressor with different inter-blade-row gaps. Journal of Thermal Science.DOI
Feng Guo-tai (2004). Numerical Investigation of the Optimal Endwall Fence Location with the Variation of Incidences. Journal of Aerospace Power.
Feng Guo-tai (2004). Numerical Investigation of the Secondary Flow Control in a Compressor Cascade Using Endwall Fences. Journal of Aerospace Power.
Zhou Fan-zhen, Guotai Feng, Hongde Jiang (2003). The Development of Highly Loaded Turbine Rotating Blades by Using 3D Optimization Design Method of Turbomachinery Blades Based on Artificial Neural Network & Genetic Algorithm. Chinese Journal of Aeronautics.DOI
Haitao Yang, Hongyan Huang, Guotai Feng, Jiexian Su, Weirong Sun (2003). Numerical Simulation of Rotor Clocking Effect in a Low-Speed Compressor. Chinese Journal of Aeronautics.DOI
Hongyan Huang, Haitao Yang, Guotai Feng, Zhongqi Wang (2003). Fully Clocking Effect in a Two-Stage Compressor.DOI
Songtao Wang, Zhongqi Wang, Guotai Feng (2001). Numerical Simulation of 3D Flow Field Structure in Turbine Cascade With Bowed Blades. Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.DOI
Feng Guo-tai (2001). Solution of Euler equation using high order accurate schemes. Ha'erbin gongye daxue xuebao.