王建华

[1]  2021.9~2021.9， 98.02-02.12德国斯图加特大学，能源工程学院，热流体机械研究所，工学博士（Dr.-Ing.)

[2]  2021.9~2021.9， 1983.09-1986.07 哈尔滨工业大学，动力工程系，工学硕士

[3]  2021.9~2021.9， 1978.02-1982.02 合肥工业大学，精密机械工程系，工学学士

[4]  78.02-82.02 合肥工业大学，精密机械工程系，工学学士

[5]  83.09-86.07 哈尔滨工业大学，动力工程系，工学硕士

[6]  98.02-02.12 德国斯图加特大学，能源工程学院，热流体机械研究所，工学博士（Dr.-Ing.）

[1]  2021.9~2021.9， ASME/IGTI Heat Transfer ，Committee Member ，社会工作

[2]  2021.9~2021.9， ASME/HTD Gas Turbine Heat Transfer (K-14) ，Committee Member ，社会工作

[3]  2021.9~2021.9， 《航空动力学报》编辑委员会 ，成员 ，社会工作

[4]  2021.9~2021.9， 98.04-02.12德国斯图加特大学，热流体机械研究所，从事强化冷却技术实验研究 ，全职研究伙伴 (Wissenschaftliche Mitarbeiterin BatA2)

[5]  2021.9~2021.9， 96.06-96.12香港城市大学，从事数学模型和数值计算方法研究 ，资深助理研究员（SR）

[6]  2021.9~2021.9， 92.02-93.08德国宇航院哥庭根流体力学研究所，从事实验流体力学先进测量技术研究 ，中科院访问学者

[7]  92.02-93.08德国宇航院哥庭根流体力学研究所，从事实验流体力学先进测量技术研究，中科院访问学者

[8]  96.06-96.12香港城市大学，从事数学模型和数值计算方法研究，资深助理研究员（SR）

[9]  98.04-02.12德国斯图加特大学，热流体机械研究所，从事强化冷却技术实验研究，全职研究伙伴 (Wissenschaftliche Mitarbeiterin BatA2)

[1]  《航空动力学报》编辑委员会成员

[2]  Committee Member of ASME/HTD Gas Turbine Heat Transfer (K-14)

[3]  Committee Member of ASME/IGTI Heat Transfer

[1] 多孔介质传热传质过程的数学模型、数值模拟方法及实验技术研究

[2] 多孔介质传热传质过程的数学模型、数值模拟方法及实验技术研究

[3] 空天飞行器主动热防护技术及相关材料/结构设计问题研究

[4] 空天飞行器主动热防护技术及相关材料/结构设计问题研究

[5] 强化冷却结构多场耦合问题实验技术及数值模拟方法研究

[6] 强化冷却结构多场耦合问题实验技术及数值模拟方法研究

[7] 现代化光学诊断及数字图像处理技术在热物理量测量方面的应用

[8] 现代化光学诊断及数字图像处理技术在热物理量测量方面的应用

[9] 新能源、洁净能源基础理论及应用技术研究

[10] 新能源、洁净能源基础理论及应用技术研究

[1] Weilong Wu, Huazhao Xu*, Jianhua Wang*, Xianyu Wu, Lei Wang, Numerical Investigation on the Influences of Pin-Fin on Cooling Air Flow of Turbine Blade Trailing Edge, ASME Paper, GT 2019-91989 June 17-21, 2019 in Phoenix, Arizona, USA..2021,

[2] Wei Song, Ming Wang, Taiqiu Liu, Zhineng Du, Huazhao Xua*, Xiaofang Cheng, Jianhua Wang*, Numerical investigation on Cooling Air Flow and Resistance Characteristics inner Laminated Cooling Structures, ASME Paper, GT2019-92025 June 17-21, 2019 in Phoenix, Arizona, USA..2021,

[3] Ran Yao, Jian-hua Wang*, Numerical Investigation on the Differences between Temperature Ratio and Density Ratio in Film-cooled Endwall, ASME Paper, GT 2018-75255 June 11-15, 2018, Oslo, Norway..2021,

[4] Peng Wang, Jian Pu*, Ren-bin Yu, Jian-hua Wang, Bo Wan, Jian-Xia Luo, Shu-qing Tian, An experimental investigation on internal flow characteristics in a realistic and entire coolant channel with ribs and film holes, ASME Paper, GT2018-75715 June 11-15, 2018, Oslo, Norway..2021,

[5] Kang Qian, Yadong Wu，Zihe Zhou, Nan Wu, Fei He*, Jianhua Wang, Meng Wang,An Experimental Investigation on the Analogous Transpiration Cooling Utilizing Hydrogels as Coolants, The 4th International Conference on Mechanical and Aero-nautical Engineering (ICMAE) Dec. 2018, id : C017..2021,

[6] Meng Wang, Fei He*, Nan Wu, Jianhua Wang, Guangqi Dong, Numerical Simulation of Transpiration Cooling within Variable Property of Water and Steam, The 4th International Conference on Mechanical and Aeronautical Engineering (ICMAE) Dec. 2018, Hong Kong, id : C018..2021,

[7] Ran Yao, Jianhua Wang*, Wenshuo Yang, Wei Wang, Zhineng Du, Ming Wang, A Numerical Investigation on the Differences between Annular and Flat Film Cooled Endwalls, ASME Paper, GT2017-63337, June 26-30, 2017, Charlotte, NC, USA..2021,

[8] Wei Wang, Jian Pu, Rui-ming Yuan, Jian-hua Wang, Bin-peng Kang, Yong-xian Ruan, An experimental investigation on the overall cooling performances of two turbine endwall structures, ASME GT2017-63226, June 26-30, 2017, Charlotte, NC, USA..2021,

[9] N Wu, J H Wang*, L Shen, G Q Dong and J H Xie, Numerical study of a three dimensional interaction between two bow shock waves and the aerodynamic heating on a wedge shaped nose cone, ICMAE [C]187, 2016 Dec. 29-31, Hong Kong..2021,

[10] Lin Shen, Jianhua Wang*, Wenjie Dong, A numerical investigation on aero-thermodynamic characteristics of a nose cone in wind tunnel and near space flight environment, International Conference on Computational Methods for Thermal Problems, [C] 220-223, 2016 July 6-8, Georgia Tech, Atlanta, USA..2021,

[1] wangjianhua ,丁锐,hefei,伍楠,飞行器及其壳体总成,201910193253.8,2019-06-04,

[2] wangjianhua ,丁锐,hefei,伍楠,高超声速飞行器及其前缘热防护结构,201810870515.5,2019-01-01,

[3] wangjianhua ,伍楠,hefei,丁锐,基于梯度多孔材料的高超声速飞行器前缘热防护方法,201810205982.6,2018-08-21,

[4] wangjianhua ,伍楠,hefei,丁锐,自适应局部激活发汗冷却的高超声速前缘热防护方法,201810205981.1,2018-08-24,

[1] 尖锐前缘发汗冷却热防护方法研究,完成,

[2] CJ高压涡轮叶片PIV流场试验,进行,

[3] 源代码研究,进行,

[4] 多孔渗透结构传质特性检测技术研究,进行,

[5] 发汗冷却试件性能测试,进行,

[6] 发散冷却的中流动与换热问题研究,完成,

[7] 先进燃气透平组合冷却技术中的流-固-热耦合问题研究,进行,

[8] 发散冷却在高超声速飞行器中应用的基础问题研究,完成,

[9] 发散冷却技术的基础问题研究,完成,

[10] 发散冷却技术的基础研究,完成,

[1] 传热传质学（双语课）,

[2] 热过程的数值模拟,

[3] 气体动力学,

[4] 传热及流动过程的数值计算方法,

[5] 基础流体力学,