Hydrodynamics of Robotic Fish Schooling
How phase and formation shape the hydrodynamic benefit of swimming in a group (2025–present)
How phase and formation shape the hydrodynamic benefit of swimming in a group (2025–present)
Ph.D. thesis work — live birds flying through a controlled vortex street (2020–2025) 
An instrumented airfoil surfing a controlled vortex street, and a model that predicts its lift (2022–2025) 
Independent control of flapping, wing folding and wing twist — featured by National Geographic
Proportional aerodynamic control on a wind turbine blade section (2019–2023)
Independently controlled, compliant wing ornithopter (2018–2019) 
Direct force controlled propulsion system for aggressive maneuvering 
Published in China Patent, 2016
Recommended citation: S. Hao, F. Yang, X. Jiang, T. Li. Distributed Vectored Propulsion System[P]. CN105151292B. 2.2016 https://patents.google.com/patent/CN105151292B/
Published in China Patent, 2016
Recommended citation: S. Hao, F. Yang, X. Jiang. Distributed Vectored Propulsion Mechanism [P]. CN205034337U. 7.2016 https://patents.google.com/patent/CN205034337U/
Published in China Patent, 2018
Recommended citation: S. Hao, F. Yang, P Tang, Y. Feng, H. Li. Omnidirectional Gimbaled Mechanism based on Ring Gear [P]. CN107117288A. 9.2018 https://patents.google.com/patent/CN107117288B/
Published in Advanced Materials Technologies, 2019
Recommended citation: X. Li, Y. Yang, B. Xie, M. Chu, H. Sun, S. Hao, Y. Chen, Y. Chen. 3D Printing of Flexible Liquid Sensor Based on Swelling Behavior of Hydrogel with Carbon Nanotubes [J]. Advanced Materials Technologies, 2019, 4(2): 1800476. https://doi.org/10.1002/admt.201800476
Published in AIAA SCITECH 2022 Forum, 2022
Recommended citation: Siyang Hao, John Cooney, Neal Fine and Kenny S. Breuer. Using an Active Gurney Flap to Modify the Performance of a Wind Turbine Wing Section [C]. SCITECH 2022 Forum. AIAA 2022-2293 https://doi.org/10.2514/6.2022-2293
Published in AIAA SCITECH 2023 Forum, 2023
Wind tunnel experiments over Re = 160,000–414,000 show that proportional deployment of an active Gurney flap improves lift and pitching moment with an increased lift-to-drag ratio, with the maximum effect near 70 degrees of deployment.
Recommended citation: S. Hao, A. Koh-Bell, R. Irani, J. Kirsch-Posner, K. Breuer. Proportional Control of Aerodynamic Forces using an Active Gurney Flap on a Wind Turbine Blade Section [C]. AIAA SCITECH 2023 Forum, AIAA 2023-0459. https://doi.org/10.2514/6.2023-0459
Published in Proceedings of the National Academy of Sciences, 2024
Combining wind tunnel flight tests, kinematic tracking and metabolic measurements on European Starlings to quantify the energetic benefit of trailing positions in small flocks.
Recommended citation: S. I. Friman, C. R. Elowe, S. Hao, L. Mendez, R. Ayala, I. Brown, C. Hagood, Y. Hedlund, D. Jackson, J. Killi, G. Orfanides, E. Ozcan, J. Ramirez, A. R. Gerson, K. S. Breuer, T. L. Hedrick. It pays to follow the leader: Metabolic cost of flight is lower for trailing birds in small groups [J]. PNAS, 2024, 121(26): e2319971121. https://doi.org/10.1073/pnas.2319971121
Published in Journal of the Royal Society Interface, 2025
Experiments with bats and a bat-inspired flapping robot show that clapping the wings during the upstroke enhances lift generation while improving power economy.
Recommended citation: X. Fan, A. Bortoni, S. Hao, S. Swartz, K. Breuer. Upstroke wing clapping in bats and bat-inspired robots offers efficient lift generation [J]. Journal of the Royal Society Interface, 2025, 22(223): 20240590. https://doi.org/10.1098/rsif.2024.0590
Published in Wind Energy, 2025
Real-time, proportional deployment of an active Gurney flap near the trailing edge of a wind turbine blade section is used to modulate lift and pitching moment, with the aerodynamic response scaling with deployment angle.
Recommended citation: S. Hao, A. Koh-Bell, R. Irani, J. Kirsch-Posner, K. Breuer. Proportional Control of Aerodynamic Forces Using an Active Gurney Flap on a Wind Turbine Blade Section [J]. Wind Energy, 2025, 28(10): e70056. https://doi.org/10.1002/we.70056
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Workshop, University of Southern California, Department of Aerospace and Mechanical Engineering, 2015