Numerical simulation on flow field and infrared characteristics of chevron nozzles

[1] Saiyed N, Mikkelsen K L, Bridges J. Acoustics and thrust of separate-flow exhaust nozzles with mixing devices for high-bypass-ratio engines .NASA TM 2000-209948, 2000 [2] Bridges J, Wernet M P.Turbulence measurements of separate flow nozzles with mixing enhancement features . AIAA-2002-2484, 2002 [3] Bridges J E, Brown C A. Parametric testing of chevrons on single flow hot jets . AIAA-2004-2824, 2004 [4] Engblom W A, Khavaran A, Bridges J.Numerical prediction of chevron nozzle noise reduction using WIND-MGBK methodology .AIAA 2004-2979, 2004 [5] Leonard B P. A stable and accurate convective modeling procedure based on quadratic upstream interpolation[J]. Computer Methods in Applied Mechanics and Engineering, 1979,19: 59-98 [6] Yakhot V, Orzag S A. Renormalization group analysis of turbulence: basic theory[J]. Journal of Scientific Computing, 1986,1: 3-11 [7] Sigel R, Howell J R. Thermal radiation heat transfer[M].3rd ed. Washington: Hemisphere Inc, 1996:385-395 [8] Solovjov V P,Webb B W.An efficient method for modeling radiative transfer in multicomponent gas mixtures with soot[J].Journal of Heat Transfer, 2001, 123:450-457