Calculation of heat transfer rates to gas turbine blades
暂无分享,去创建一个
[1] S. Shamroth,et al. Assessment of a transitional boundary layer theory at low hypersonic Mach numbers , 1972 .
[2] R. W. Fish,et al. Practical calculations of transitional boundary layers , 1973 .
[3] P. Bradshaw,et al. Applications of a General Method of Calculating Turbulent Shear Layers , 1972 .
[4] J. A. Pope,et al. Convective Heat Transfer to Gas Turbine Blade Surfaces , 1954 .
[5] Richard D. Lander,et al. External Heat-Transfer Distribution on Film Cooled Turbine Vanes , 1972 .
[6] R. Antonia,et al. Calculation of a Turbulent Boundary Layer Downstream of a Step Change in Surface Temperature , 1979 .
[7] A. Townsend,et al. Self-preserving flow inside a turbulent boundary layer , 1965, Journal of Fluid Mechanics.
[8] N. W. Foster. Film cooling of gas turbine blades , 1976 .
[9] E. Markland,et al. Heat transfer to turbine blading in the presence of secondary flow , 1965 .
[10] A. E. Forest. Engineering predictions of transitional boundary layers , 1977 .
[11] Self-preserving development within turbulent boundary layers in strong adverse pressure gradients , 1965 .
[12] A. B. Turner,et al. Local Heat Transfer Measurements on a Gas Turbine Blade , 1971 .
[13] P. Bradshaw. Effects of Streamline Curvature on Turbulent Flow. , 1973 .
[14] A. Townsend,et al. Equilibrium layers and wall turbulence , 1961, Journal of Fluid Mechanics.