Ge Zhou | Astronautics | Best Researcher Award

Dr. Ge Zhou | Astronautics | Best Researcher Award

Nanjing University of Aeronautics and Astronautics | China

Ge Zhou, a dedicated researcher from Weifang, Shandong, has built a strong academic and professional foundation in the field of aeronautics and astronautics. He earned his degree in Aircraft Power Engineering from the Civil Aviation University of China, where his research focused on aeroacoustic analysis of counter-rotating rotors. He later pursued advanced studies at the Nanjing University of Aeronautics and Astronautics in Energy and Power Engineering, centering his work on the bird strike motion law and internal flow characteristics of turboprop engine inlets. Currently, he continues his academic journey in Aeronautical and Astronautical Sciences and Technology at the same university, exploring the mechanism of boundary layer interference of droplets during the rain ingestion process of serpentine inlets. Alongside his education, Ge Zhou has accumulated significant research and project experience. He has contributed to numerical analysis and validation technology of turboprop aircraft main engine exclusion characteristics, where his responsibilities included studying bird, sand, and ice foreign object exclusion, conducting multidisciplinary integrated optimization design, and developing a comprehensive verification test system. Additionally, he has worked on aerodynamic interference calculations for a UAV tilt-rotor aircraft, analyzing interactions between fuselage and rotor during hovering, transition, and cruise states. Through his focused research, technical expertise, and commitment to advancing aero-engine safety and performance, Ge Zhou demonstrates strong potential to make lasting contributions to the field of aeronautical engineering.

Profile: Orcid 

Featured Publications 

"Experimental Study of Foreign Object Exclusion Characteristics of a Bifurcated Turboprop Inlet"

"Experimental Study of Aerodynamic and Bird Exclusion Characteristics of a Branched Turboprop Inlet Under Ground Suction Conditions"

"Aerodynamic study of a bifurcated turboprop engine inlet with a propeller for flow at ground suction conditions"

"Ice Object Exclusion Characteristics of Turboshaft Engine Inlet under Helicopter/Inlet Integration Conditions"