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Numerical Simulation Study of NACA2415 Airfoil Using PANS Model Based on User-Defined Functions

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DOI: 10.23977/jemm.2025.100102 | Downloads: 20 | Views: 575

Author(s)

Yu Yunyun 1, Yang Tianhe 1, Zhou Daqing 2

Affiliation(s)

1 School of Air Transportation and Engineering, Nanhang Jincheng College, Nanjing, China
2 College of Energy & Electrical Engineering, Hohai University, Nanjing, China

Corresponding Author

Yu Yunyun

ABSTRACT

This paper constructs a Partially-Averaged Navier-Stokes (PANS) turbulence model using User-Defined Function (UDF) programming based on FLUENT software and applies it to the numerical simulation study of the NACA2415 airfoil. Through the secondary development of FLUENT, the construction and validation of the PANS model were successfully achieved. The flow field characteristics of the NACA2415 airfoil at different angles of attack were calculated, and the lift coefficient was monitored and compared with wind tunnel experimental results. The study showed that the PANS model effectively captures the velocity streamlines and pressure variations on the surface of the airfoil, demonstrating a high predictive accuracy compared to experimental data. This research provides a technical reference for the simulation of complex flow fields and the optimization of turbulence modeling methods.

KEYWORDS

UDF, PANS, NACA2415, Numerical Simulation

CITE THIS PAPER

Yu Yunyun, Yang Tianhe, Zhou Daqing, Numerical Simulation Study of NACA2415 Airfoil Using PANS Model Based on User-Defined Functions. Journal of Engineering Mechanics and Machinery (2025) Vol. 10: 13-22. DOI: http://dx.doi.org/10.23977/jemm.2025.100102.

REFERENCES

[1] Girimaji, S. S. Partially-averaged Navier–Stokes model for turbulence: a Reynolds-averaged Navier–Stokes to direct numerical simulation bridging method [J]. Journal of Applied Mechanics, 2006, 73(3), 413-421.
[2] Basara, B., Girimaji, S. S., & Jakirlić, S. PANS methodology applied to elliptic-relaxation based eddy-viscosity turbulence model [J]. International Journal of Heat and Fluid Flow, 2011,32(3), 508-519.
[3] Huang Biao, Wang Guoyu, Quan Xiaobo, Chen Guanghao. Application of PANS Model in Cavitating Turbulent Flow Numerical Calculation. Journal of Applied Mechanics, 2011, 28(4): 339-344.
[4] Du Ruofan, Yan Chao, Luo Dahai. Performance Analysis of PANS Method in Numerical Simulation of Flow Around Twin Cylinders. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(8): 1503-1509.
[5] Wang Peng, Li Ming, Wang Wei. Comparison of SAS and PANS Models in Flow around a Cylinder. Journal of Aerodynamics, 2019, 37(4): 530-538.
[6] Abbott, I. H., & von Doenhoff, A. E. Summary of Airfoil Data[M]. NACA Report No. 824.1959.
[7] G. K. Batchelor, An Introduction to Fluid Dynamics[M]. Cambridge, UK: Cambridge University Press, 2000
[8] Yu Yunyun, Zhou Daqing, Yu An, et al. Numerical Simulation of Cavitation Characteristics in an Axial Flow Pump Based on the Modified PANS Model[J]. Journal of Drainage and Irrigation Machinery Engineering, 2022, 40(12): 1204-1211.
[9] Huang R, Luo X, Ji B, et al. Turbulent flows over a backward facing step simulated using a modified Partially-Averaged Navier-Stokes model [J]. Journal of Fluids Engineering, 2017, 139(4):044501.
[10] Launder B.E, Spalding D.B, Lectures in Mathematical Models of Turbulence[M]. Academic Press, London, 1972.
[11] Davidson L. The PANS k-epsilon model in a zonal hybrid RANS-LES formulation[J]. International Journal of Heat & Fluid Flow, 2014, 46(4):112-126.  
[12] Chen, S., & Zhang, X. A modified PANS approach for the simulation of unsteady flow and cavitation in turbomachinery [J]. Journal of Fluid Engineering, 2020, 142(3), 031301. 
[13] Doe, J., & Smith, A. Experimental Study of Subsonic Flow Past a Body of Revolution[J]. Journal of Fluid Mechanics, 2020, 250(3), 453-467.

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