1.Acharya M.,Metwally H.(1992) “Usteady Pressure Field and Vorticity Production over a Pitching Airfoil“,AIAA J.,VOL. 30,No.2
2.Ahsanul M.,Acharya M.(1994) “Suppression of Dynamic-Stall Vortices over Pitching Airfoils by Leading-Edge Suction“,AIAA J.,Vol32,No.8
3.Badran, B.;McCormick, S.,Gursul, I.(1998) “Control of leading-edge vortices with suction“, J. of Aircraft,Vol.35,No.1
4.Carr L. W. (1988) “ Progress in Analysis and Prediction of Dynamic Stall “, J. of Aircraft, Vol.25, No.1。
5.Carr L. W., Chandrasekhara M. S. (1992) “ Design and Development of a Compressible Dynamic Stall Facility “, J. of Aircraft, Vol.29, No.3。
6.Chang C. C., Chern R. L. (1991) ” A numerical study of flow around an impulsively started circular cylinder by a deterministic vortex method “, J. Fluid Mech., Vol.233, pp.243-263。
7.Cowley, S. J.,Van Dommenlen,L.,(1990) “On the Lagrangian Description of Unsteady Boundary-Layer Separation“,J. of Fluid Mechanics,Vol. 210,pp593~645
8.Francis,M.S.,Keesee,J. E.,(1985) “Airfoil Dynamic Stall Performance with Large-Amplitude Motion“,AIAA J.,Vol.23,No.11
9.Ericsson L. E., Reding J. P. (1984) “ Unsteady Flow Concepts for Dynamic Stall Analysis “, J. of Aircraft, Vol.21, No.8。
10.Farnborough (1990) “ British Pilot Lauds Performance of Su-27 “, Aviation Week & Space Technology, September 24。
11.McCormick, S.,Gursul, I.(1996) “Effect of shear-layer control on leading-edge vortices. “,J. of Aircraft ,Vol.33,No.6.
12.McCroskey W. J., Carr L. W., McAlister K. W. (1976) “ Dynamic Stall Experiments on Oscillating Airfoils “, AIAA J., Vol.14, No1。
13.Parmenter K.,Rockwell D.(1990)“Transient Response of Leading-Edge Vortice to Localized Suction “,AIAA J.,Vol.28,No.6
14.Shih C., Lourenco L., Dommelen L. V., Krothapalli A. (1992) “ Unsteady Flow Past an Airfoil Pitching at a Constant Rate “, AIAA J., Vol.30, No.5。
15.Shih C., Ho C. M. (1994) “ Vorticity balance and time scals of a two-dimensional airfoil in an unsteady free stream “, Phys. Fluid, Vol.6, No.2。
16.Strickland J. H., Graham G. M. (1986) “ Dynamic Stall Inception Correlation for Airfoils Undergoing Constant Pitch Rate Motions ”, AIAA J., Vol.24, No.4。
17.Strickland J. H., Graham G. M. (1987) “ Force Cofficients for a NACA-0015 Airfoil Undergoing Constant Pitch Rate Motions ”, AIAA J., Vol.25, No.4。
18.Visbal,M. R.,Shang,J. S.(1989) “Investigation of the Floe Structure Around a Rapidly Pitching Airfoil“,AIAA J.,Vol.27,No.8
19.Walker J. M., Helin H.E., and Strickland J.H. (1985) ” An Experimental Investigation of an Airfoil Undergoing Large-Amplitude Pitching Motions “, AIAA J., Vol.23, No.8。
20.郭光輝 (1990) “ 三角翼前緣渦漩之實驗研究 “, 臺灣大學應用力學所碩士論文。21.廖茂君 (1992) “ 作俯仰運動的二維橢柱體之流場分析 “, 臺灣大學應用力學所碩士論文。
22.蕭穎謙 (1993) “ 環繞機翼之二維渦漩流的研究 “, 臺灣大學應用力學所博士論文。23.謝錦坤 (1997) “ 入流渦列與俯仰機翼交互作用之實驗分析 “,中興大學機械所碩士論文。24.陳大志 (1997) “ 縱向非定常運動之機翼流場的實驗與數值研究 “, 臺灣大學應用力學所碩士論文。25.江俊杰(1998) “具俯仰及縱向非定常運動之高攻角二維機翼流場實驗與數值研究“, 臺灣大學應用力學所碩士論文。