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Faning Shao

Nanjing University of Aeronautics and Astronautics

Yudao Street

210016

Nanjing,, 210016

China

  • Nanjing University of Aeronautics and Astronautics

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Dynamic Blade Tip Clearance Control of Aero-Engine by the Integration of Cooling Air with Fuel Thermal Management System

Number of pages: 30 Posted: 05 Jun 2024
weilong gou, Shiyu Yang, Yuanfang Lin, Faning Shao, Xingang Liang and Bo Shi
Nanjing University of Aeronautics and Astronautics, Tsinghua University, Tsinghua University, Nanjing University of Aeronautics and Astronautics, Tsinghua University and Nanjing University of Aeronautics and Astronautics
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Abstract:

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aero-engine, multi-system transient simulation, tip clearance control, thermal management, performance optimization