Thermal Effects on the Normal Shock Dynamics in a Laval Nozzle

作者: Hui Cao , Lipo Wang , Qiang Zhang , Xiang Li

DOI: 10.2514/1.J056734

关键词: NozzleShock frontGas constantMechanicsThermalAerodynamicsBoundary layer thicknessShock (mechanics)Dynamics (mechanics)Materials science

摘要:

参考文章(6)
V. Jaunet, J. F. Debiève, P. Dupont, Length Scales and Time Scales of a Heated Shock-Wave/Boundary-Layer Interaction AIAA Journal. ,vol. 52, pp. 2524- 2532 ,(2014) , 10.2514/1.J052869
R. Maffulli, L. He, Wall Temperature Effects on Heat Transfer Coefficient for High-Pressure Turbines Journal of Propulsion and Power. ,vol. 30, pp. 1080- 1090 ,(2014) , 10.2514/1.B35126
N. Stosic, On heat transfer in screw compressors International Journal of Heat and Fluid Flow. ,vol. 51, pp. 285- 297 ,(2015) , 10.1016/J.IJHEATFLUIDFLOW.2014.10.026
M.P. Martín, E.M. Taylor, M. Wu, V.G. Weirs, A bandwidth-optimized WENO scheme for the effective direct numerical simulation of compressible turbulence Journal of Computational Physics. ,vol. 220, pp. 270- 289 ,(2006) , 10.1016/J.JCP.2006.05.009
David M. Dawson, Sanjiva K. Lele, Large Eddy Simulation of A Three-DimensionalCompression Ramp Shock-Turbulent Boundary Layer Interaction 53rd AIAA Aerospace Sciences Meeting. ,(2015) , 10.2514/6.2015-1518
Matteo Bernardini, I Asproulias, J Larsson, S Pirozzoli, F Grasso, None, Heat transfer and wall temperature effects in shock wave turbulent boundary layer interactions Physical Review Fluids. ,vol. 1, pp. 084403- ,(2016) , 10.1103/PHYSREVFLUIDS.1.084403