References
- Platzer, M.F., Jones, K.D., and Young J., "Flapping Wing Aerodynamics: Progress and Challemges", AIAA Journal, Vol. 46, No. 9, 2008, pp. 2136-2149. https://doi.org/10.2514/1.29263
- Isogai, K., Shinmoto, Y., and Watanabe Y., "Effects of Dynamic Stall on Propulsive Efficiency and Thrust of Flapping Airfoil", AIAA Journal, Vol. 37, No. 10, 1999, pp. 1145-1151. https://doi.org/10.2514/2.589
- Birnbaum, W., "Das ebene Problem des Schlagenden Fluegels", Zeitschrift fuer Angewandte Mathematik und Mechanical, Vol. 4, No. 4, 1924, pp. 277-292. https://doi.org/10.1002/zamm.19240040401
- Garrick, I.E., "Propulsion of a Flapping and Oscillating Airfoils", NACA Rept. 567, 1936.
- Jones, K.D., Dohring, C.M., and Platzer, M.F., "Experimental and Computational Investigation of the Knoller-Benz Effect", AIAA Journal, Vol. 36, No. 7, 1998, pp. 1240-1246. https://doi.org/10.2514/2.505
- Lai, J.C.S., and Platzer, M.F., "Jet Characteristics of a Plunging Airfoil", AIAA Journal, Vol. 37, No. 12, 1999, pp. 1529-1537. https://doi.org/10.2514/2.641
- Taylor, G.K., Nudds, R.L., and Thomas, A.L.R., "Flying and Swimming Animals Cruise at a Strouhal Number Tuned for High Power Efficiency", Nature (London), Vol. 425, Oct., 2003, pp. 707-711. https://doi.org/10.1038/nature02000
- Young, J., and Lai, J.C.S., "Oscillation Frequency and Amplitude Effects on the Wake of a Plunging Airfoil", AIAA Journal, Vol.42, No.10, 2004, pp. 2042-2052. https://doi.org/10.2514/1.5070
- Rival, D., and Tropea, C., "Characteristics of Pitching and Plunging Airfoils under Dynamic-Stall Conditions", Journal of Aircraft, Vol. 47, No. 1, 2010, pp. 80-86. https://doi.org/10.2514/1.42528
- Moryossef, Y., and Levy, Y., "Effect of Oscillations on Airfoils in Close Proximity to the Ground", AIAA Journal, Vol. 42, No. 9, 2004, pp. 1755-1764. https://doi.org/10.2514/1.6380
- Wagner, C., Huttl, T., and Sagaut, P., Large-Eddy Simulation for Acoustics, CAMBRIDGE UNIVERSITY PRESS, 2007.
- Wilcox, D.C., Turbulence Modeling for CFD, 2nd., DCW Industries Inc., California, 2000.
- Kim, J.W., and Lee, D.J., "Optimizes Compact Finite Difference Schemes with maximum Resolution", AIAA Journal, Vol. 34, No. 5, 1986, pp. 887-893.
- Sandberg, R.D., Jones, L.E., and Sandham, N.D., "A Zonal Characteristic Boundary Condition for Numerical Simulations of Aerodynamic Sound", ECCOMA CFD, 2006.
- Kim, T.S., and Kim, J.S., "Numerical Analysis of the Three Dimensional Wake Flow and Acoustic Field around a Circular Cylinder", Int. J. of Aeronautical and Space Sciences, Vol. 11, No. 4, 2010, pp. 319-235. https://doi.org/10.5139/IJASS.2010.11.4.319
- Blake, W.K., "Dipole Sound from Cylinders", Mechanics of Flow induced Sound and Vibration, Vol. 1, Academic Press, New York, 1986, pp. 219-287.
- Williamson, C.H.K., "Three Dimensional Wake Transition", Journal of Fluid Mechanics, Vol. 328, 1996, pp. 345-407. https://doi.org/10.1017/S0022112096008750
- Yoo, J.K., and Kim, J.S., "Analysis of Unsteady Oscillating Flow around Two Dimensional Airfoil at High Angle of Attack", J. Comput. Fluids Eng., Vol. 18, No. 1, 2013, pp. 1-6. https://doi.org/10.6112/kscfe.2013.18.1.001
- Liu, Y., Li, K., Zhang, J., Wang, H., and Liu, L., "Numerical Bifurcation Analysis of Static Stall of Airfoil and Dynamic Stall under Unsteady Perturbation", Commun Nonlinear Sci Numer Simulat, Vol. 17, No. 8, 2012, pp. 3427-3434. https://doi.org/10.1016/j.cnsns.2011.12.007
-
Critzos, C.C., Heyson, H.H., and Boswinkle, R.W.," Aerodynamic Characteristics of NACA0012 Airfoil Section at the Angle of Attack from
$0^{\circ}$ to$180^{\circ}$ ", NACA TN 3361, 1955. - Craig, A.P., and Hansman, R.J., "An Experimental Low Reynolds Number Comparison of a Wortmann FX67-K170 Airfoil, a NACA0012 Airfoil, and a NACA 64-210 Airfoil in Simulated Heavy Rain", NACA CR 181119, 1987.
- Hoerner, S.F., and Borst, H.V., Fluid Dynamic Lift, Horerner Fluid Dynamics, U.S.A., 1985, pp. 2-17 - 4-26.