The data from a series of flow experiments is given to you for analysis. Refrigerant-22 is flowing at a velocity of 0.043m/s and a bulk temperature of 370K over an isothermal plate at 290K. Some thermo-physical properties are shown in the table below. Thermal Conductivity [W/m/K] 0.06728 Kinematic Viscosity [m2/s] Prandtl Number [-] 1.235*10-7 3.28 If the transition from laminar to turbulent flow is determined to happen at the end of the plate: A. What is the length of the plate? B. What are the hydrodynamic and thermal boundary layer thicknesses at the end of the plate? C. What is the heat transfer rate per plate width for the entire plate? Given the plate length you determined in part A above is increased by 50%, at the end of the extended plate, what are D. Reynolds number? E. Hydrodynamic and thermal boundary layer thicknesses?
The data from a series of flow experiments is given to you for analysis. Refrigerant-22 is flowing at a velocity of 0.043m/s and a bulk temperature of 370K over an isothermal plate at 290K. Some thermo-physical properties are shown in the table below. Thermal Conductivity [W/m/K] 0.06728 Kinematic Viscosity [m2/s] Prandtl Number [-] 1.235*10-7 3.28 If the transition from laminar to turbulent flow is determined to happen at the end of the plate: A. What is the length of the plate? B. What are the hydrodynamic and thermal boundary layer thicknesses at the end of the plate? C. What is the heat transfer rate per plate width for the entire plate? Given the plate length you determined in part A above is increased by 50%, at the end of the extended plate, what are D. Reynolds number? E. Hydrodynamic and thermal boundary layer thicknesses?
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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