CFD Analysis of Oscillating Airfoil during Pitch Cycle

Abstract:

This research paper presents the CFD analysis of oscillating airfoil during pitch cycle. Unsteady subsonic flow is simulated for pitching airfoil at Mach number 0.283 and Reynolds number 3.45 millions. Turbulent effects are also considered for this study by using K-ω SST turbulent model. Two-dimensional unsteady compressible Navier-Stokes code including two-equation turbulence model and PISO pressure velocity coupling is used. Pressure based implicit solver with first order implicit unsteady formulation is used. The simulated pitch cycle results are compared with the available experimental data.

• Periodical: Applied Mechanics and Materials (Volumes 152-154)
• Pages: 906-911
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.152-154.906
• Online since: January 2012
• Authors: Ahmad Kamran, Zhi Gang Wu, Muhammad Amjad Sohail
• Keywords: Angle of Attack, Centre of Pressure, Pitching Moment Coefficient, Subsonic Flow, Turbulence Model

References

[1] D. G. Mabey, 1999. Unsteady Aero-dynamics: Restrospect and prospect, Aero-nautical Journal, Vol. 103, No. 1019, Review Paper No. 003, 1 - 18.

[2] W. J. McCroskey, 1982. Unsteady airfoils, Ann. Rev. Fluid Mech., Vol. 14, 285 - 311.

DOI: 10.1146/annurev.fl.14.010182.001441

[3] W. J. McCroskey, 1988. Some Rotorcraft Applications of Computational Fluid Dynamics, NASA TM 100066.

[4] W. Shyy, M. Berg and D. Lyungvist, 1999. Flapping and Flexible Wings for Biological and Micro Air Vehicles, Progress in Aerospace Sciences, Vol. 35, No. 5, pp.455-505.

DOI: 10.1016/s0376-0421(98)00016-5

[5] T. J. Mueller(ed. ), 2001. Fixed and Flapping Wing Aerodynamics for Micro Air Vehicles, Progress in Aeronautics and Astronautics, AIAA, Reston, VA, Vol. 195.

[6] S. Yang, S. Luo and F. Liu, 2006. Optimization of Unstalled Pitching and Plunging Motion of an Airfoil, AIAA paper, submitted to 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 1055.

DOI: 10.2514/6.2006-1055

[7] T. Theodorsen, 1934. General theory of aerodynamic instability and the mechanism of flutter, NACA REPORT No. 496.

[8] I. E. Garrick, 1936. Propulsion of a flapping and oscillating airfoil, NACA Report No. 567.

[9] I. H. Tuncer and M. F. Platzer, 2000. Computational study of flapping airfoil Aerodynamics, Journal of Aircraft, Vol. 37, pp.514-520.

DOI: 10.2514/2.2628

[10] K. Isogai, Y. Shinmoto and Y Watanabe, 1999. Effects of Dynamic Stall on Propulsive Efficiency and Thrust of Flapping Airfoil, AIAA Journal, Vol. 37, pp.1145-1151.

DOI: 10.2514/3.14303

[11] Ramamurti, R. and Sandberg, W., 2001. Simulation of Flow about Flapping Airfoils using Finite Element Incompressible Flow Solver, AIAA Journal, Vol. 39, p.253 – 260.

DOI: 10.2514/3.14725

[12] J. M. Anderson, K. Streitlien, D. S. Barrett and M.S. Triantafyllou, 1998. Oscillating foils of high propulsive efficiency,J. Fluid Mech., 360, pp.41-72.

DOI: 10.1017/s0022112097008392

[13] K. Siva Kumar, Sharanappa V. Sajjan " Unsteady Flow past a Combined Pitching and Plunging Aerofoil using an Implicit RANS Solver 2011 International Conference on Mechanical and Aerospace Engineering (CMAE 2011).

DOI: 10.4028/www.scientific.net/amm.110-116.3481

[14] R.I. Issa. Solution of Implicitly Discretized Fluid Flow Equations by Operator Splitting. Journal of Computational. Physics., 62: 40-65, (1986).

DOI: 10.1016/0021-9991(86)90099-9