Professional Appointment
May, 2014 - present Research associate
Oct., 2011 - April, 2014 Post-doctoral researcher
Department of Aeronautics and Astronautics
College of Engineering, Peking University, China
Sept., 2007 – Jan., 2010 Assistant specialist
Department of Mechanical and Aerospace Engineering
University of California, Irvine, United States
Education
Ph.D. July, 2011 Department of Fluid Mechanics
Northwestern Polytechnical University, Xi’an, Shaanxi, China
BEng July, 2005 School of Aeronautics
Northwestern Polytechnical University, Xi’an, Shaanxi, China
Research Interests
fluid mechanics of Turbomachinery, computational fluid dynamics, design optimization
Academic Services
Member of ASME, AIAA
Reviewer of J Propul. Power, ASME Turbo Expo, etc.
Projects
1. National Natural and Science Foundation of China (Grant No. 51206003), 2013.01-2015.12, PI
2. National Science Foundation for Post-doctoral Scientists of China (Grant No. 2013T60035), PI
3. National Science Foundation for Post-doctoral Scientists of China (Grant No. 2012M510267), PI
4. National Natural and Science Foundation of China (Grant No. 51376009), 2014.01-2017.12,
PI: Feng Liu
5. Alstom Power of Switzerland, “Design Optimization of a Supersonic Steam Turbine Blade”, 2007.09-
2009.12, PI: Feng Liu
6. Beijing Center of COMAC, “Calculation and Prediction of the Buffet Boundary and Loading of C919”,
2012.01-2013.12, PI: Feng Liu
Publications
J1. Luo Jiaqi *, and Liu Feng. Multi-Objective Optimization of a Transonic Compressor Rotor by Using an Adjoint
Method. to appear in AIAA Journal
J2. Luo Jiaqi *, Liu Feng, and McBean Ivan. Aerodynamic Optimization of a Turbine Blade Row through Endwall
Contouring by an Adjoint Method. to appear in Journal of Propulsion and Power
J3. Luo Jiaqi *, Zhou Chao, and Liu Feng. Multi-Point Design Optimization of a Transonic Compressor Blade by
Using an Adjoint Method. ASME Journal of Turbomachinery, 2014, 136(5): 051005 (doi: 10.1115/1.4025164)
J4. Luo Jiaqi, Xiong Juntao, and Liu Feng. Aerodynamic Design Optimization by Using a Continuous Adjoint Method.
SCIENCE CHINA Physics, Mechanics & Astronomy, 2014, 57(7): 1363-1375 (doi: 10.1007/s11433-014-5479-0)
J5. Luo Jiaqi *, and Liu Feng. Gradient-Based Response Surface Approximation for Design Optimization. Acta
Physica Sinica, 2013, 62(19): 190201 (doi: 10.7498/aps.62.190201)
J6. Luo Jiaqi, Xiong Juntao, Liu Feng, and McBean Ivan. Three-Dimensional Aerodynamic Design Optimization of a
Turbine Blade by Using an Adjoint Method. ASME Journal of Turbomachinery, 2011, 133(1): 011026 (doi: 10.1115/1.4001166)
C1. Luo Jiaqi, and Liu Feng. Multi-Objective Design Optimization of a Transonic Compressor Rotor Using an Adjoint Equation
Method. AIAA Paper 2013-2732, June 24-27, 2013, San Diego, California, United States (doi: 10.2514/2013-2732)
C2. Luo Jiaqi, Zhou Chao, and Liu Feng. Multi-Point Design Optimization of a Transonic Compressor Blade by
Using an Adjoint Method. Proceedings of the ASME Turbo Expo 2013, Vol. 6B, pp. V06BT37A030 (doi: 10.1115/GT2013-95155)
C3. Luo Jiaqi, Liu Feng, and McBean Ivan. Optimization of Endwall Contours of a Turbine Blade Row Using an
Adjoint Method. Proceedings of the ASME Turbo Expo 2011, Vol. 7, pp: 1335-1350 (doi: 10.1115/GT2011- 46163)
C4. Luo Jiaqi, Xiong Juntao, Liu Feng, and McBean Ivan. Secondary Flow Reduction by Blade Redesign and
Endwall Contouring Using an Adjoint Equation Method. Proceedings of the ASME Turbo Expo 2010, Vol. 7,
pp: 547-562 (doi: 10.1115/GT2010-22061)
C5. Luo Jiaqi, Xiong Juntao, Liu Feng, and McBean Ivan. Three-Dimensional Aerodynamic Design Optimization
of a Turbine Blade by Using an Adjoint Method. Proceedings of the ASME Turbo Expo 2009, Vol. 7, pp: 651-
664 (doi: 10.1115/ GT2009-60115)
* the corresponding author
Academician
