个人简介： 马姗，女，1988.01生。工学博士，毕业于西北工业大学、动力工程及工程热物理专业；主持或参研国家自然科学基金项目2项，四川省科技厅项目2项，民航飞行技术与飞行安全重点实验室项目2项，校级科研项目4项，校级教研项目1项，横向项目2项；以第一作者或通讯作者身份在国内外各高水平学术刊物上公开发表SCI/EI论文20余篇，授权发明专利、实用新型专利近30项；获四川省第二届教学创新竞赛三等奖1项，四川省第三届教学创新竞赛二等奖1项，四川省第四届教学创新竞赛二等奖1项，校级教学建设一等奖1项；公开出版本科生教材《飞行原理》。主讲本科生《空气动力学》、《飞行原理》、《飞行性能与配载计划》等专业课程，参与研究生课程《飞行性能与运行》的讲授及建设工作。
主要研究成果： [1]A Combined Application of Micro-vortex Generator and Boundary Layer Suction in a High-load Compressor Cascade. Chinese Journal of Aeronautics[J]. Chinese Journal of Aeronautics,2019. [2]Study of Combined Flow Control Strategies Based on a Quantitative Analysis in a High-Load Compressor Cascade[J]. Aerospace Science and Technology,2019. [3]Effects of Modified Micro-vortex Generators on Aerodynamic Performance in a High-load Compressor Cascade[J].Proc IMechE, Part A: Journal Power and Energy,2019. [4]Effects of segmented layer suction slot and micro-vortex generator on a high-load compressor cascade performance[J].Proc IMechE, Part C: Journal of Mechanical Engineering Science,2021. [5]Applications of little blades in a high-load compressor cascade with leaned blade[J].Proc IMechE, Part C: Journal of Mechanical Engineering Science,2021. [6]Optimization study on the influence of little blades’ spatial position on a compressor cascade performance[J].Proc IMechE, Part G: Journal of Aerospace Engineering,2022. [7]Influence of a Wavy Blade-End Applied in an Axial Compressor Cascade on the Secondary Flow of the Passage[J].Journal of Applied Fluid Mechanics, 2022. [8]Comparative Study of the Performance Improvement of an Axial Compressor with a Micro-Vortex Generator and a Suction Slot[J].Journal of Applied Fluid Mechanics, 2023. [9]Unsteady characteristics analysis of compressors based on the proper orthogonal decomposition method[J].AIP Advances,2025.
|
