Comparison of Pressure Distribution of Naca 0012 Between CFD Code and Experimental
DOI:
https://doi.org/10.37934/cfdl.14.2.3541Keywords:
CFD, Euler equationAbstract
Computational Fluid Dynamics (CFD) is a tool to solve engineering problem. Commercial CFD code are being used most engineering problem but rarely for external aerodynamic problem due some limitation of features. Compare to in house CFD code that able to written in certain area of interest and also implement specific discretization scheme to increase accuracy. In this work, the CFD code are developed by using high resolution scheme (ROE scheme and TVD scheme) for flow past through airfoil NACA 0012. Experimental result of wind tunnel is obtained from literature which are from Gregory and O’Reilly at Mach number M = 0.13 for different values of angle of attack at α= 0° and α = 10°. Another wind tunnel result from Haris at Mach number = 0.8 for different angles of attack α= 0° and α= 3.86°. Comparison results from the both codes indicate that developed CFD code by using TVD scheme able to give the closest result for both experimental.
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Hu, Zhe, Wenyong Tang, Hongxiang Xue, Xiaoying Zhang, and Jinting Guo. "Numerical simulations using conserved wave absorption applied to Navier–Stokes equation model." Coastal engineering 99 (2015): 15-25. https://doi.org/10.1016/j.coastaleng.2015.02.007
Chen, Gui-Qiang G., Jun Chen, and Mikhail Feldman. "Stability and asymptotic behavior of transonic flows past wedges for the full Euler equations." Interfaces and Free Boundaries 19, no. 4 (2018): 591-626. https://doi.org/10.4171/IFB/394
Vos, J. B., Arthur Rizzi, D. Darracq, and E. H. Hirschel. "Navier–Stokes solvers in European aircraft design." Progress in Aerospace Sciences 38, no. 8 (2002): 601-697. https://doi.org/10.1016/S0376-0421(02)00050-7
Kroll, Norbert, Datta Gaitonde, and Michael Aftosmis. "A systematic comparative study of several high resolution schemes for complex problems in high speed flows." In 29th Aerospace Sciences Meeting, p. 636. 1991. https://doi.org/10.2514/6.1991-636
Chen, Ming‐Hsiung, Chen‐Chi Hsu, and Wei Shyy. "Assessment of TVD schemes for inviscid and turbulent flow computation." International journal for numerical methods in fluids 12, no. 2 (1991): 161-177. https://doi.org/10.1002/fld.1650120205
Rosly, Nurhayati, Qamarul Ezani Kamarudin, and Bambang Basuno. "Comparative Study on Various Numerical Schemes for Solving Nozzle Flow Problems." CFD Letters 12, no. 6 (2020): 93-106. https://doi.org/10.37934/cfdl.12.6.93106
Gu, Kai Xuan, Zhi Qiang Li, Jun Jie Wang, Yuan Zhou, Hong Zhang, Bing Zhao, and Wei Ji. "The effect of cryogenic treatment on the microstructure and properties of Ti-6Al-4V titanium alloy." In Materials science forum, vol. 747, pp. 899-903. Trans Tech Publications Ltd, 2013. https://doi.org/10.4028/www.scientific.net/MSF.747-748.899
Yusop, Fatimah, Bambang Basuno, and Zamri Omar. "Application of Modified 4th Order Runge Kutta-TVD Scheme for the Flow Past through Symmetrical Model." In Applied Mechanics and Materials, vol. 315, pp. 181-185. Trans Tech Publications Ltd, 2013. https://doi.org/10.4028/www.scientific.net/AMM.315.181
Chung, T. J. Computational fluid dynamics. Cambridge university press, 2002. https://doi.org/10.1017/CBO9780511606205
Hoffmann, Klaus A., and Steve T. Chiang. "Computational fluid dynamics volume I." Engineering Education System (2000).
Chang, Yu-Li. Development of a CFD code using TVD schemes and advanced turbulence models for incompressible flow simulations. Michigan Technological University, 1997.
Blazek, Jiri. Computational fluid dynamics: principles and applications. Butterworth-Heinemann, 2015. https://doi.org/10.1016/B978-0-08-099995-1.00012-9
van Leer, Bram. "An introduction to the article “Reminiscences about difference schemes” by SK Godunov." Journal of Computational Physics 153, no. 1 (1999): 1-5. https://doi.org/10.1006/jcph.1999.6270
Gregory, Nigel, and C. L. O'reilly. "Low-speed aerodynamic characteristics of NACA 0012 aerofoil section, including the effects of upper-surface roughness simulating hoar frost." (1970).
Harris, Charles D. Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8 foot transonic pressure tunnel. No. NASA-TM-81927. 1981.
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