论文信息 - Application of laminar boundary layer heat transfer theory to low thrust rocket nozzles - 字舞流文

Application of laminar boundary layer heat transfer theory to low thrust rocket nozzles

[1] P. F. Massier,et al. Some observations on reduction of turbulent boundary-layer heat transfer in nozzles. , 1966 .

[2] M. Sibulkin. HEAT TRANSFER TO AN INCOMPRESSIBLE TURBULENT BOUNDARY LAYER AND ESTIMATION OF HEAT-TRANSFER COEFFICIENTS AT SUPERSONIC NOZZLE THROATS , 1956 .

[3] Ernest Mayer. Analysis of Convective Heat Transfer in Rocket Nozzles , 1961 .

[4] A. B. Witte,et al. Prediction of heat transfer from laminar boundary layers, with emphasis on large free- stream velocity gradients and highly cooled walls. , 1966 .

[5] Lloyd H. Back,et al. Convective heat transfer in a convergent-divergent nozzle , 1964 .