1、 国家级一流本科课程-传热学,教育部,2/6,2025
2、 航空发动机高温旋转部件流动与换热测试技术,国防科学技术进步一等奖,工信部,5/20,2021
3、 立德树人优秀奖,教学成果奖,北京航空航天大学,1/1,2020
4、 校级优秀班主任,教学成果奖,北京航空航天大学,1/1,2019
5、 第十五届“我爱我师”十佳教师,教学成果奖,北京航空航天大学,1/1,2016
发明专利
[1] 罗翔,宋凯峰,刘冬冬,邬泽宇,张伟佳,李泽丰,郭帅;专利名称:一种航空发动机预旋叶片通道流通面积可调的供气装置;专利号:CN202512000853.6
[2] 罗翔,邬泽宇,张哲,刘冬冬;专利名称:一种采用液态金属的回热系统;专利号:CN202411024297.5
[3]罗翔,白阳,邬泽宇,刘冬冬,徐国强;专利名称:一种基于流动自模化的盘腔实验特征参数推广应用方法;专利号:CN202410243456.4
[4] 罗翔,何建,白阳,刘冬冬;专利名称:一种用于压气机的变管径减涡器及其减涡系统;专利号:CN202210448970.2
[5] 罗翔,刘品良;专利名称:具备导引结构的叶片、转子以及叶片设计方法;专利号:CN202210164500.3
论文
[1] Wang Y , Hu T , Dong S , Wu, Z. , Luo, X. , & Guo, L. Applicable imputation of highly causal temporal and coupled missing temperature time series in a rotating cavity using generative adversarial networks[J].Thermal science and engineering progress, 2025:63.DOI:10.1016/ j.tsep.2025. 103689.
[2] Wang S , Luo X , Guo L ,et al. Experimental and computational investigation on flow characteristics of rotating cavities with high inlet pre-swirl axial throughflow[J].Chinese Journal of Aeronautics, 2024, 37(4):276-293.DOI:10.1016/j.cja.2024.01.017.
[3] Bai Y , Luo X , Liu D ,et al. Flow characteristics of radial inflow in impeller rear cavity with baffle plate[J].Chinese Journal of Aeronautics, 2024, 37(2):270-282.DOI:10.1016/j.cja.2023.10.005.
[4]Sealing efficiency performance of four different rim seals in turbine cavity[J]. Chinese Journal of Aeronautics, 2024, 37(12):347-357.DOI:10.1016/j.cja.2024.07.034.
[5] Zhang Z , Wang S , Luo X ,et al. Windage Torque and Flow Characteristics of a Co-Rotating Conical Cavity Under Radial Inflow[J]. 2023.DOI:10.2139/ssrn.4660886.