Parametric Study of Compressible Turbulent Spots
作者： J. A. Redford , N. D. Sandham , G. T. Roberts
DOI: 10.1007/978-90-481-3652-0_84
关键词:
摘要: The compressible Navier–Stokes equations are solved for turbulent spots at Mach 3 and 6, with both adiabatic cold (T w = T ∞ ) wall boundary conditions on a flat plate. From the results spot growth propagation rates derived which will help to quantify length of laminar transition. simulations also yield skin-friction heat-transfer data.
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Frank M. White, Viscous Fluid Flow ,(1974)
Kenneth S Breuer, None, The Evolution of a Localized Disturbance in a Laminar Boundary Layer Laminar-Turbulent Transition. pp. 189- 198 ,(1990) , 10.1007/978-3-642-84103-3_16
Shi Chang Zhang, Gary L Messing, Wayne Huebner, YBa2Cu3O7−x Superconductor powder synthesis by spray pyrolysis of organic acid solutions Journal of Aerosol Science. ,vol. 22, pp. 585- 599 ,(1991) , 10.1016/0021-8502(91)90014-9
Kenneth S Breuer, Joseph H Haritonidis, None, The evolution of a localized disturbance in a laminar boundary layer. Part 1. Weak disturbances Journal of Fluid Mechanics. ,vol. 220, pp. 569- 594 ,(1990) , 10.1017/S002211209000338X
Brian Cantwell, Donald Coles, Paul Dimotakis, Structure and entrainment in the plane of symmetry of a turbulent spot Journal of Fluid Mechanics. ,vol. 87, pp. 641- 672 ,(1978) , 10.1017/S0022112078001809
MICHAEL C. FISCHER, Spreading of a turbulent disturbance. AIAA Journal. ,vol. 10, pp. 957- 959 ,(1972) , 10.2514/3.50265
L. KRISHNAN, N. D. SANDHAM, Effect of Mach number on the structure of turbulent spots Journal of Fluid Mechanics. ,vol. 566, pp. 225- 234 ,(2006) , 10.1017/S0022112006002412