UFR 2-03 References
Flow around oscillating airfoil
Underlying Flow Regime 2-03 © copyright ERCOFTAC 2004
References
[1] E. Stanewsky, “Shock Boundary Layer Interaction”, in Boundary Layer Simulation and Control in Wind Tunells, AGARD-AR-224, April 1988, pp 271-305.
[2] E. Stanewsky, D. Basler, “Experimental Investigation of Buffet Onset and Penetration on a Supercritical Airfoil at Transonic Speeds”. AGARD CP 483, 1990 pp. 4-1,4-13.
[3] G. Barakos, D. Drikakis, “Numerical Simulation of Transonic Buffet Flows Using Various Turbulence Closures”, Int. J. Of Heat and Fluid Flow 21 (2000) pp.620-626.
[4] I. Abbott and A. Von Doenhoff, Theory of Wing Sections, Dover Pub., New York, 1959.
[5] S.R. Bland AGARD Two-Dimensional Aeroelastic Configurations. AGARD-AR-156, Aug.1979.
[6] S.S. Davis, Data Set 2, NACA 64A010 (NASA AMES MODEL) Oscillatory Pitching in AGARD-R-702 Advisory Report No. 702 .Compedium of Unsteady Aerodynamic MeasurementsAugust 1982, pp 2-1, 2-22.
[7] S.S. Davis and G. Malcolm, Experimental Unsteady Aerodynamics of Conventional and Supercritical Airfoils. NASA TM-81221, Aug 1980.
[8] G. Barakos, D.Drikakis, Implicit Unfactored Method for Unsteady Turbulent Compressible Flows with Moving Boundaries, Computer and Fluids 28 (1999) 899-922.
[9] WH Guo, DX Fu, YW Wa, Numerical Investigation of dynamic stall of an oscillating aerofoil. Int J Meth Fluids 1994; 19(8): 723-34.
[10] N.C. Lambourne, General review, Advisory Report No. 702 .Compedium of Unsteady Aerodynamic MeasurementsAugust 1982, pp 0-1, 0-22.
[11] W.J. Chyu, S.S. Davis, K.S. Chang, Calculation of Unsteady Transonic Flow over an aerofoil, AIAA Journal, Vol.19.No6. June 1981 pp 684-690.
[12] F. Liu, S. Ji, Unsteady Flow Calculations with a Multigrid Navier-Stokes Method, AIAA Journal, 34, No.10, October 1996 pp2047-2053.
[13] R.Beam and R.F. Warming, An Implicit Finite Difference Algorithm for Hypersonic Systems in Conservation Law Form, Journal of Computational Physics, Vol 22, Sept, 1976, pp. 87-110.
[14] J. Steger, Implicit Finite Difference Simulation of Flow About Arbitrary Two-Dimensional Geometries, AIAA Journal, Vol. 16, July 1978, pp. 679-686.
[15] S.S. Davis and G. Malcolm, Transonic Shock-Wave/Boundary Layer Interactions on an Oscillating Airfoil, AIAA Journal, Vol.18, Nov. 1980, pp. 1306-1312.
[16] S.S. Davis and G. Malcolm, Unsteady Aerodynamics of Conventional and Supercritical Airfoil, AIAA Paper 78-257, 1978.
[17] A. Jameson, Time Dependent Calculations Using Multigrid, with Applications to Unsteady Flows Past Airfolis and Wings, AIAA Paper 91-1596, June 1991.
[18] G. Barakos, D. Drikakis, Implicit-unfactored implementation of two-equation turbulence models in Compressible Navier-Stokes methods. Inter. Journal Meth. Fluids 1998, 28 pp 73-94.
[19] G. Barakos, D. Drikakis, Assesment of Various Low-Reynolds number turbulence models in shock-boundary layer interaction., Comput. Meth Eng, 1998, 160 (1-2) pp 155-174.
[20] S. Fan, B. Lakshminaryana, M. Barnett, Low-Reynolds number k-ε model for unsteady turbulent boundary-layer flows. AIAA J. 1993, 31 (10), 1777-17784.
[21] Zhang H, Regio M, Trepanier J Y, Camaresso R, Discrite form of the GCL for the moving meshes and its implementation in CFD schemes, Computer and Fluids 1993, 22 (1):9-23.
© copyright ERCOFTAC 2004
Contributors: Joanna Szmelter - Cranfield University