Studies on the enhancement of aerodynamic performance in aerofoils using co-flow jet: a comprehensive review

The purpose of this study is to present a detailed review of the co-flow jet (CFJ) method applied to improve the aerodynamic performance of aircraft. This active flow control technique has been extensively implemented in fixed and rotary wings, wind turbines and ducts to improve aerodynamic performa...

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Published inAerospace systems (Online) Vol. 6; no. 1; pp. 1 - 14
Main Authors Balaji, K., Wessley, G. Jims John
Format Journal Article
LanguageEnglish
Published Singapore Springer Nature Singapore 01.03.2023
Subjects
Aerospace Technology and Astronautics
Engineering
Review
Space Exploration and Astronautics
Space Sciences (including Extraterrestrial Physics
Aerodynamic performance
Co-flow jet
RANS
Aerofoil
Simulation
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Abstract The purpose of this study is to present a detailed review of the co-flow jet (CFJ) method applied to improve the aerodynamic performance of aircraft. This active flow control technique has been extensively implemented in fixed and rotary wings, wind turbines and ducts to improve aerodynamic performance while reducing the weight, drag and runway distance. Almost all the works in simulations found in the reported literature are performed using CFD software mostly using RANS solver, while a few other solvers have also been reported. Very few experimental studies on aerodynamic performance improvement using wind tunnels are available on the CFJ mechanism. The parameters under study include injection and suction velocity, injection and suction diameter, Reynolds number, Mach number, etc., applied to different phases of flight aiming at delaying the flow separation. This review facilitates the understanding of the research gap that exists in using an active flow control mechanism in the CFJ method.
AbstractList The purpose of this study is to present a detailed review of the co-flow jet (CFJ) method applied to improve the aerodynamic performance of aircraft. This active flow control technique has been extensively implemented in fixed and rotary wings, wind turbines and ducts to improve aerodynamic performance while reducing the weight, drag and runway distance. Almost all the works in simulations found in the reported literature are performed using CFD software mostly using RANS solver, while a few other solvers have also been reported. Very few experimental studies on aerodynamic performance improvement using wind tunnels are available on the CFJ mechanism. The parameters under study include injection and suction velocity, injection and suction diameter, Reynolds number, Mach number, etc., applied to different phases of flight aiming at delaying the flow separation. This review facilitates the understanding of the research gap that exists in using an active flow control mechanism in the CFJ method.
Author Wessley, G. Jims John
Balaji, K.
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  surname: Wessley
  fullname: Wessley, G. Jims John
  organization: Department of Aerospace Engineering, Karunya Institute of Technology and Sciences
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Co-flow jet
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Snippet The purpose of this study is to present a detailed review of the co-flow jet (CFJ) method applied to improve the aerodynamic performance of aircraft. This...
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SubjectTerms Aerospace Technology and Astronautics
Engineering
Review
Space Exploration and Astronautics
Space Sciences (including Extraterrestrial Physics
Title Studies on the enhancement of aerodynamic performance in aerofoils using co-flow jet: a comprehensive review
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