Tongtong Meng , Xin Li , Xinyu Ren , Ling Zhou , Lucheng Ji
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引用次数: 0
Abstract
In this manuscript, to simultaneously inhibit multiple causes of corner separation and therefore improve the flow around endwall as much as possible, the combined control by both Full Blended Blade and Endwall (Full-BBEW) and endwall Vortex Generator (VG) are studied. Firstly, a Full-BBEW design is built for a linear cascade and then an combined control is carefully designed by placing a VG in the middle passage of Full-BBEW design. Both numerical and experimental analyses over the entire working condition are performed. Results demonstrate that the combined design significantly reduces overall aerodynamic losses across the full range of design Mach number, with a more pronounced effect observed at high incidence angles. The combined BBEW and VG design provides a comprehensive control strategy that mitigates corner separation and improves endwall flow, resulting in improved aerodynamic performance.
期刊介绍：
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.
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