Driver, D. M. and Seegmiller, H. L., "Features of Reattaching Turbulent Shear Layer in Divergent Channel Flow," AIAA Journal, Vol. 23, No. 2, Feb 1985, pp. 163-171.
McCroskey, W. J., "A Critical Assessment of Wind Tunnel Results for the NACA 0012 Airfoil," NASA TM 100019, October 1987
Ladson, C. L., "Effects of Independent Variation of Mach and Reynolds Numbers on the Low-Speed Aerodynamic Characteristics of the NACA 0012 Airfoil Section," NASA TM 4074, October 1988
A. M. Savill. "Some recent progress in the turbulence modeling of bypass transition. Near-Wall Turbulent Flows," Elsevier Science Publishers, pp. 829-848,1993.
P.E. Roach, D.H. Brierley. "The influence of a turbulent free stream on zero pressure gradient transitional boundary layer development. Part I: Test Cases T3A and T3B," Simulation of Unsteady and Transition to Turbulence. Cambridge University Press. Cambridge, pp. 319-347, 1992.
Three element airfoil - Download supporting material
Moir I.R.M. "Measurements on a Two-Dimensional Airfoil with High-Lift Devices," AGARD AR 303. Aug 1994. Case A2.
Nelson, T.E., Godin, P., De Rango, S. and Zingg, D.W. "Flow Computations for a Three-Element Airfoil System," Canadian Aeronautics and Space Journal, Vol. 45, No. 2, June 1999.
De Rango, S. and Zingg, D.W. "Higher-Order Spatial Discretization for Turbulent Aerodynamics Computations,"" AIAA Journal, Vol. 39, No. 7, July 2001.
Fejtek, I. "Summary of Code Validation Results for a Multiple Element Airfoil Test Case," AIAA 28th Fluid Dynamics Conference, Snowmass Village, CO, USA, 29 June 1997 - 02 July 1997.
Cook, P.H., M.A. McDonald, M.C.P. Firmin. "Aerofoil RAE 2822 - Pressure Distributions, and Boundary Layer and Wake Measurements. Experimental Data Base for Computer Program Assessment," AGARD Report AR 138, 1979.
Kline, S. J., Cantwell, B. J., Lilley, G. M. 1980-81 AFOSR-HTTM-Stanford Conference on Complex Turbulent Flows: Comparison of Computation and Experiment. Stanford University, Stanford, California, 1982.
F. Wattendorf. "A Study of the Effect of Curvature on Fully Developed Turbulent Flows." PhD Thesis, California Institute of Technology, US. June, 1934.
Static mixer - Swirling flow - Download supporting material
N. Mansour, J. Kim, P. Moin. Reynolds-Stress and Dissipation Rate Budgets in a Turbulent Channel Flow. NASA TM 89451. 1987.
Click here to download
J. Kim, P. Moin, R. Moser. Turbulence statistics in fully developed channel flow at low Reynolds number. Journal of Fluid Mechanics, 177, 133-166. 1987.
Click here to download