个人简述:

2014年12月获得国防科技进步三等奖；2014年12月获得航天学院先进工作者；2015年8月获得优秀本科毕业设计指导教师。

科研工作:

围绕火箭发动机设计、仿真过程，集中研究设计方法，结构、流场及燃烧仿真过程。先后主持国防基础课题、总装预研课题、航天支撑课题及工程应用课题十余项，参与自然基金课题及其它课题9项。发表学术论文7篇，其中SCI检索1篇，EI检索6篇。 [1]     Wei-Hua Hui Fu-Ting Bao Xiang-Geng Wei Yang liuAnalysis of Ablative Performance of C/C Composite Throat Containing Defects Based on X-ray 3D Reconstruction in a Solid Rocket Motor, International Journal of Turbo & Jet-Engines. ISSN (Online) 2191-0332, ISSN (Print) 0334-0082,(DOI:10.1515/tjj-2015-0021)[2]     惠卫华,鲍福廷,刘旸. 弹器水面燃气分离时机原则探讨及计算验证[J]. 宇航学报,2014,02:157-162.(EI Index: 20141317523707)[3]     惠卫华,鲍福廷,刘旸. 考虑低燃温燃气发生器试验的弹射器内弹道性能预示[J]. 固体火箭技术,2013,06:715-719. (EI Index: 20140817349812)[4]     惠卫华,鲍福廷,刘旸,阎海生. 弹器水面分离燃气弹射内弹道性能分析及系统实现[J]. 固体火箭技术,2013,02:161-164+184. (EI Indes: 20132516429215)[5]     Hui, Wei-Hua Bao, Fu-Ting Hu, Hai-Feng Liu, Yang, Research on the thermal buckling analysis of the attitude liquid rocket engine with film cooling[C], Mechanical and Aerospace Engineering IV, 2013 390, 714-719.(EI Index:20134016817547)[6]     Hui, Wei-Hua Bao, Fu-Ting Liu, Yang, Analysis and implementation of the separation trajectory equations of different launch environments, 2013 IEEE 3rd International Conference on System Engineering and Technology, ICSET 2013, 67-72.(EI Index:20140117155520)[7]     Hui, Weihua, Measurement system of α β surface radioactive contamination based on virtual training, IEEE 2011 10th International Conference on Electronic Measurement and Instruments, ICEMI 2011, 90-93.(EI Index:20114414464675)[8]     夏冰戈,鲍福廷,惠卫华,刘旸,刘强. 考虑燃烧恒面性和结构完整性的翼柱形药柱形状优化[J]. 固体火箭技术,2013,05:620-625.(EI Index: 20140417238126)