（1）燃气轮机传热与冷却技术

（2）涡轮叶片气动及传热

（3）气动传热测量技术等

（4）非定常传热机理及应用

（1）涡轮叶片典型冷却结构流阻及换热特性试验研究 主持在研

（2）涡轮叶片典型冷却单元及其组合结构的传热与流阻特性试验研究 主持在研

（3）航空科学基金：小间隙跨音速高压涡轮叶尖传热特性实验研究 主持已结题

（4）自然科学基金：气冷涡轮叶尖泄漏流动的高低速模化设计及实验研究 主持已结题

（5）自然科学基金：气冷涡轮动叶叶顶多目标拓扑优化研究 参与在研

（6）自然科学基金：高负荷悬臂静叶间隙流影响多级压气机气动性能的机理研究 参与在研

（7）国家科技重大专项：过渡态涡轮叶尖换热特性数值模拟及试验技术研究 参与在研

（8）上海市科技创新专项：陶瓷基复合材料高压涡轮导叶热分析及冷却设计技术研究 参与在研

（1）Lu S， Zhang, Q*, He li. A HIGH-SPEED DISK ROTOR RIG DESIGN FOR TIP AEROTHERMAL RESEARCH [J]. Journal of Turbomachinery, 2021

（2）Lu S*, Ma H, Zhang Q, et al. Cutback squealer tip trailing edge cooling performance[J]. International Journal of Heat and Mass Transfer, 2020, 154: 119632.

（3）Lu S*, Deng Q, Ligrani P M, et al. Effects of coolant and wall temperature variations on impingement jet array thermal performance[J]. Numerical Heat Transfer, Part A: Applications, 2020: 1-15.

（4）Wang W, Lu S*, Jiang H, et al. Influence of tip clearance and cavity depth on heat transfer in a cutback squealer tip[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, 235(8):095441002096469

（5）Zhu D, Zhang Q, Lu S*, et al. RELATIVE CASING MOTION EFFECT ON SQUEALER TIP COOLING PERFORMANCE AT TIGHT TIP CLEARANCE[J]. Journal of Thermal Science and Engineering Applications, 2020: 1-18.

（6）Jiang H, Zhang Q, He L, Lu S*,et al. Experimental Evidence of Temperature Ratio Effect on Turbine Blade Tip Heat Transfer[J]. Journal of Turbomachinery, 2018, 140(12).

（7）Zhang B, Qiang X*, Lu S, et al. Numerical investigations of unsteady passing wake effects on turbine blade tip aerothermal performance with different tip clearances[J]. International Journal of Numerical Methods for Heat & Fluid Flow, 2019.

（8）Qian M, Lu S*, Zhang B, et al. Effect of Squealer Rim Slot Structure on Turbine Blade Aerothermal Performance[C]//Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2019, 58646: V05AT13A005.

（9）Tang M, Lu S*, Liu Y, et al. Aerothermal characteristics of transonic over-tip leakage flow for different tip geometries with cooling injection[J]. Aerospace Systems, 2019, 2(2): 189-196.

（10）Zhang B, Qiang X*, Teng J, Lu S. Unsteady Passing Wake Effects on Turbine Blade Tip Aerodynamic and Aerothermal Performance With Film Cooling[C]//Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2019, 58653: V05BT22A002.

（11）王维杰, 卢少鹏*, 马海腾, 等. 高压涡轮尾切凹槽叶尖冷却换热特性[J]. 航空动力学报, 2019, 34(10): 2131-2139.

（12）D. Zhu, S. Lu*, H. Ma, Q. Zhang, J. Teng. Rotating Effect on Transonic Squealer Tip Cooling Performance. Turbomachinery Technical Conference and Exposition GT2017 June 26-30, 2017, Charlotte, NC, USA,GT2017-64293

（13）Lu S, Qiang X, Wen F, Teng J. Aerodynamic and Heat Transfer Optimization of One Stage Air-Cooled Turbine[C]//ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2015: V02CT45A014-V02CT45A014.

（14）卢少鹏, 迟重然, 王龙飞. 涡轮静叶叶型与气膜孔优化对气动与冷却性能影响[J]. 航空动力学报, 2014, 29(6): 1301-1311.

（15）卢少鹏, 迟重然, 罗磊. 气热耦合条件下涡轮静叶三维优化[J]. 推进技术, 2014 (3): 356-364.

（16）《燃气涡轮气动优化设计体系》   2019.09 哈尔滨工业大学出版社