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Hengtao Shi*, Rui Zhu, Zidong Yu, Jiao Wang. Influence of Hub Cap Shape on Axial Fan Rotor Root Flow Separation: An Analytical Model for Quick Design. Physics of Fluids. (accepted)
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Shi Hengtao*, Yu Xianjun*. A Stage Flow Parameter Analytical Model for Transonic Counter-Rotating Compressor and Its Application. Aerospace. 2023; 10(2):144
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Hengtao Shi, Baojie Liu, Xianjun Yu. Criteria for designing low-loss and wide operation range variable inlet guide vanes.Aerospace Science and Technology,2018,80:177-191
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​施恒涛*, 王蛟. 跨声速对转压气机叶型和掠形对流场及气动特性的调控优化机制研究, 推进技术. 2024, 已录用，online
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Hengtao Shi*. A Parametric Blade Design Method for High-Speed Axial Compressor, Aerospace, 2021, 8(9): 271
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Hengtao Shi*, Bo Song and Jiao Wang. Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification. Int J Turbo Jet Eng. 2024, Accepted and Online.
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吴森，于贤君，施恒涛，刘宝杰. 变循环压缩系统单外涵模式外涵节流特性分析.热能动力工程.2021,36(11),34-40.
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Hengtao Shi, Xianjun Yu. A Stage Flow Parameter Analytical Model for Transonic Counter-Rotating Compressor and Its Application. Aerospace 2023, 10, 144.
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施恒涛, 刘宝杰, 于贤君. 基于多项式的曲率连续前缘造型方法及应用, 航空动力学报. 2020, 35(2):397-409
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Baojie Liu, Hengtao Shi,Xianjun Yu. A new method for rapid shock loss evaluation and reduction for the optimization design of a supersonic compressor cascade, Proc IMechE Part G: Journal of Aerospace Engin
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Hengtao Shi, Lucheng Ji. Leading edge redesign of dual-peak type variable inlet guide vane and its effect on aerodynamic performance, Proc IMechE Part G: Journal of Aerospace Engineering,2021,235(9):1077-1
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