LES of Film Cooling for Different Jet Fluids
The present paper investigates the impact of the velocity and density ratio on the turbulent mixing process in gas turbine blade film cooling. A cooling fluid is injected from an inclined pipe at α=30° into a turbulent boundary layer profile at a freestream Reynolds number of Re∞ =400,000.This jet-in-a-crossflow (JICF) problem is investigated using large-eddy simulations (LES). The governing equations comprise the Navier-Stokes equations plus additional transport equations for several species to simulate a non-reacting gas mixture. A variation of the density ratio is simulated by the heat-mass transfer analogy, i.e., gases of differentdensity are effused into an an air crossflow at a constant temperature. An efficient large-eddy simulation method for low subsonic flows based on an implicit dual time-stepping scheme combined with low Mach number preconditioning is applied. The numerical results and experimental velocity data measured using two-component particle-image velocimetry (PIV) are in excellent agreement. The results show the dynamics of the flow field in the vicinity of the jet hole, i.e., the recirculation region and the inclination of the shear layers, to be mainly determined by the velocity ratio. However, evaluating the cooling efficiency downstream of the jet hole the mass flux ratio proves to be the dominant similarity parameter,i.e., the density ratio between the fluids and the velocity ratio have to be considered.
LES jet-in-a-crossflow film cooling density ratio velocity ratio cooling efficiency
P.Renze W.Schr(o)der M.Meinke
Aerodynamisches Institut, RWTH-Aachen 52062 Aachen, Germany
国际会议
昆明
英文
57-69
2006-09-18（万方平台首次上网日期，不代表论文的发表时间）