Path: Thermal/HeatExchanger
% HeatTransferCoeffTaylor Heat transfer coefficient based on Taylor The Nusselt exponent is limited for z/d < 1 to 1. The correlation is only valid for z/d > 1. Type HeatTransferCoeffTaylor for a demo Default properties are for a He/Xe mixture and an N2 gas. -------------------------------------------------------------------------- Form: d = HeatTransferCoeffTaylor [h,nU,rE,rho,pR,dP,hAve] = HeatTransferCoeffTaylor(u,d,l) -------------------------------------------------------------------------- ------ Inputs ------ u (1,1) Velocity (m/s) d (.) Data structure .p (1,1) Pressure (N/m^2) .mDot (1,1) Mass flow rate (kg/s) .tB (1,1) Bulk temperature (K) .tW (1,1) Wall temperature (K) .mu (1,1) Dynamic viscosity (Pa s) .l (1,1) Channel length (m) .d (1,1) Channel diameter (m) .a (1,1) Channel area (m^2) .lambda (1,1) Heat transfer coefficient W/(m K) .cP (1,1) Heat capacity (J/(kg K) .m (1,1) Molecular weight (kg/mol) l (1,:) Points for computing h ------- Outputs ------- h (1,:) Heat transfer coefficient (W/m^2 K) nU (1,:) Nusselt number rE (1,1) Reynold's number rho (1,1) Density (kg/m^3) pR (1,:) Prandtl number dP (1,1) Pressure drop/pressure hAve (1,1) Average heat coefficient -------------------------------------------------------------------------- Reference: Ersheng You, Lei Shi, Zuoyi Zhang,"Thermodynamics Properties of Binary Gas Mixtures for Brayton Space Nuclear Power System," Proceedings of the HTR 2014 Weihai, China, October 27-31, 2014 Paper HTR2014-61286. --------------------------------------------------------------------------
AerospaceUtils: AtmosphericCalculations/ReynoldsNumber SC: Environs/MolWt2R Thermal: HeatExchanger/PrandtlNumber Common: Graphics/Plot2D
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