The modification design of airfoil is a crucial aspect of aircraft design.Implementing corrugated structures on the lower wing surface can significantly affect the aerodynamic performance of the airfoil under specific...The modification design of airfoil is a crucial aspect of aircraft design.Implementing corrugated structures on the lower wing surface can significantly affect the aerodynamic performance of the airfoil under specific conditions.This study focuses on macroscale corrugated structures based on the Clark YM15 airfoil.A series of concave triangular corrugations were arranged on its lower surface,and various corrugated airfoil types were derived.Computational Fluid Dynamics(CFD)simulations were used to analyze the performance and flow characteristics of these corrugated airfoils,and to investigate the impact of structural parameters,quantity,and layout of the corrugations on the lift-to-drag performance of the airfoil.The results demonstrate that judiciously configured corrugated structures can enhance the lift-to-drag performance at a small angle of attack,with the double-corrugation structure showing the most significant improvement.Wind tunnel experiments were respectively conducted on the double-corrugation airfoil and the original airfoil,which validate the accuracy of the CFD simulations and confirm the lift and drag performance advantages of the corrugated airfoil over the original design.展开更多
The linear dispersion relation of a trapezoidally corrugated slow wave structure （TCSWS） is analyzed and presented. The size parameters of the TCSWS are chosen in such a way that they operate in the x-band frequency...The linear dispersion relation of a trapezoidally corrugated slow wave structure （TCSWS） is analyzed and presented. The size parameters of the TCSWS are chosen in such a way that they operate in the x-band frequency range. The dispersion relation is solved by utilizing the Rayleigh-Fourier method by expressing the radial function in terms of the Fourier series. A highly accurate synthetic technique is also applied to determine the complete dispersion characteristics from experimentally measured resonances （cold test）. Periodic structures resonate at specific frequencies when the terminals are shorted numerical calculation, synthetic technique and cold appropriately. The dispersion characteristics obtained from test are compared, and an excellent agreement is achieved.展开更多
A corrugated structure is built and tested on many FEL facilities,providing a'dechirper'mechanism for eliminating energy spread upstream of the undulator section of X-ray FELs.The wakefield effects are here st...A corrugated structure is built and tested on many FEL facilities,providing a'dechirper'mechanism for eliminating energy spread upstream of the undulator section of X-ray FELs.The wakefield effects are here studied for the beam dechirper at the Shanghai high repetition rate XFEL and extreme light facility(SHINE),and compared with analytical calculations.When properly optimized,the energy spread is well compensated.The transverse wakefield effects are also studied,including the dipole and quadrupole effects.By using two orthogonal dechirpers,we confirm the feasibility of restraining the emittance growth caused by the quadrupole wakefield.A more efficient method is thus proposed involving another pair of orthogonal dechirpers.展开更多
Corrugated steel–concrete(CSC)composite structures are increasingly used in tunnel and culvert projects due to their good mechanical properties.The design of CSC composite structures is often governed by deflection l...Corrugated steel–concrete(CSC)composite structures are increasingly used in tunnel and culvert projects due to their good mechanical properties.The design of CSC composite structures is often governed by deflection limits in service,hence it becomes crucial to evaluate accurately their flexural stiffness.In this work,the deflection deformation mechanism of CSC composite structure is studied by experimental and numerical methods,and a simplified formula for calculating the flexural stiffness is established.In addition,the deflection results obtained by different methods are compared and analyzed.It is found that:(1)the flexural stiffness of the CSC composite structure is constant only when the load is small,and after the bending moment exceeds a certain value,the flexural stiffness will gradually become smaller as the bending moment increases.(2)The value of the bending moment corresponding to the end of the elastic stage of the bending moment-deflection curve increases with the increase of the axial force in the composite structure.(3)As the axial force of the composite structure increases,the flexural bearing capacity of the structure increases first and then decreases.展开更多
基金supported by the 2023 Shanghai Industrial Collaborative Innovation Project,China(No.CXXT-2023-05).
文摘The modification design of airfoil is a crucial aspect of aircraft design.Implementing corrugated structures on the lower wing surface can significantly affect the aerodynamic performance of the airfoil under specific conditions.This study focuses on macroscale corrugated structures based on the Clark YM15 airfoil.A series of concave triangular corrugations were arranged on its lower surface,and various corrugated airfoil types were derived.Computational Fluid Dynamics(CFD)simulations were used to analyze the performance and flow characteristics of these corrugated airfoils,and to investigate the impact of structural parameters,quantity,and layout of the corrugations on the lift-to-drag performance of the airfoil.The results demonstrate that judiciously configured corrugated structures can enhance the lift-to-drag performance at a small angle of attack,with the double-corrugation structure showing the most significant improvement.Wind tunnel experiments were respectively conducted on the double-corrugation airfoil and the original airfoil,which validate the accuracy of the CFD simulations and confirm the lift and drag performance advantages of the corrugated airfoil over the original design.
文摘The linear dispersion relation of a trapezoidally corrugated slow wave structure （TCSWS） is analyzed and presented. The size parameters of the TCSWS are chosen in such a way that they operate in the x-band frequency range. The dispersion relation is solved by utilizing the Rayleigh-Fourier method by expressing the radial function in terms of the Fourier series. A highly accurate synthetic technique is also applied to determine the complete dispersion characteristics from experimentally measured resonances （cold test）. Periodic structures resonate at specific frequencies when the terminals are shorted numerical calculation, synthetic technique and cold appropriately. The dispersion characteristics obtained from test are compared, and an excellent agreement is achieved.
基金supported by the Youth Innovation Promotion Association CAS(Nos.2018300 and 2021282)the National Key Research and Development Program of China(No.2018YFE0103100)the National Natural Science Foundation of China(No.11935020)。
文摘A corrugated structure is built and tested on many FEL facilities,providing a'dechirper'mechanism for eliminating energy spread upstream of the undulator section of X-ray FELs.The wakefield effects are here studied for the beam dechirper at the Shanghai high repetition rate XFEL and extreme light facility(SHINE),and compared with analytical calculations.When properly optimized,the energy spread is well compensated.The transverse wakefield effects are also studied,including the dipole and quadrupole effects.By using two orthogonal dechirpers,we confirm the feasibility of restraining the emittance growth caused by the quadrupole wakefield.A more efficient method is thus proposed involving another pair of orthogonal dechirpers.
基金funded by Shanghai 2020“Science and Technology Innovation Action Plan”Project,China(Grant No.20dz1202600)National Natural Science Foundation of China(Grant No.52090083)+1 种基金Science and Technology Innovation and Demonstration Project of Department of Transport of Yunnan Province,China(Grant No.[2020]106)The authors gratefully acknowledge their financial supports.
文摘Corrugated steel–concrete(CSC)composite structures are increasingly used in tunnel and culvert projects due to their good mechanical properties.The design of CSC composite structures is often governed by deflection limits in service,hence it becomes crucial to evaluate accurately their flexural stiffness.In this work,the deflection deformation mechanism of CSC composite structure is studied by experimental and numerical methods,and a simplified formula for calculating the flexural stiffness is established.In addition,the deflection results obtained by different methods are compared and analyzed.It is found that:(1)the flexural stiffness of the CSC composite structure is constant only when the load is small,and after the bending moment exceeds a certain value,the flexural stiffness will gradually become smaller as the bending moment increases.(2)The value of the bending moment corresponding to the end of the elastic stage of the bending moment-deflection curve increases with the increase of the axial force in the composite structure.(3)As the axial force of the composite structure increases,the flexural bearing capacity of the structure increases first and then decreases.
