施恒涛*, 王蛟，于子冬. 梯度加速自适应粒子群分层算法的压气机叶片多工况气动优化, 推进技术. 2025，在审 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 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 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) Shi Hengtao*, Yu Xianjun*. A Stage Flow Parameter Analytical Model for Transonic Counter-Rotating Compressor and Its Application. Aerospace. 2023; 10(2):144 ​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 Hengtao Shi*. A Parametric Blade Design Method for High-Speed Axial Compressor, Aerospace, 2021, 8(9): 271 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. 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. Hengtao Shi. Parametric Research and Aerodynamic Characteristic of a Two-Stage Transonic Compressor for Turbine-Based Combined Cycle Engine. Aerospace, 2021, 9(7), 346. 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 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

施恒涛*, 王蛟，于子冬. 梯度加速自适应粒子群分层算法的压气机叶片多工况气动优化, 推进技术. 2025，已录用

Shi Hengtao*, Yu Xianjun*. A Stage Flow Parameter Analytical Model for Transonic Counter-Rotating Compressor and Its Application. Aerospace. 2023; 10(2):144

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

Hengtao Shi*. A Parametric Blade Design Method for High-Speed Axial Compressor, Aerospace, 2021, 8(9): 271

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.

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.

Hengtao Shi. Parametric Research and Aerodynamic Characteristic of a Two-Stage Transonic Compressor for Turbine-Based Combined Cycle Engine. Aerospace, 2021, 9(7), 346