Numerical simulation of transpiration cooling in porous nose cone under hypersonic conditions

Transpiration cooling in a two-dimensional porous nose cone under hypersonic flow have been numerically investigated. The numerical model intricately captures the interaction between compressible and incompressible flows in the boundary layer and the phase change of coolant within porous region. The validation of numerical method is performed by comparing the simulation results with experimental data. The simulation results are in reasonable agreement with the experimental data. The results show that the increase of blowing ratio can effectively improve the cooling efficiency of transpiration cooling,where the blowing ratio represents the mass flow rate ratio between the coolant of porous region and the mainstream free flow. Such as, the average cooling efficiency rises from 0.33 to 0.86 when the blowing ratio increases from 0.0459% to 0.2753%. Although the porous resistance force increases as the particle diameter and porosity decrease, the effect of these parameters and solid material of porous region on the cooling efficiency are marginal.