%A736 l 36.llT'UI T'UIltu CulIvtcioII Ovti a llai plalt uut iU NOW Palaliti LUthe plate:a) Laminar Flow:0.664RE/2Pr/3Nu =a) Turbulent Flow:Nu = 0.037Re*/5Pr/3Numerical Exercise1. A flat plate is supplied with a constant heat flux of 100 [W/m²]from bottom. The plate has 0.5m2 area and is kept in a room withambient temperature 20°C. If it has a steady state temperature of32°C what is the heat transfer coefficient?Ta = 293[K]ģ = h(T, – Ta)Tp = 305[K]ģ = 100 [W /m²]Numerical Exercise2. The air has the following properties at 27C: Density[kg.m-3], Dynamic ViscosityHeat capacity, Cp = 1.005 [kJ.kg-1.K-']. If the thermal conductivityof air at that temperature is 1= 0.026 [W.m-'.K-'], what is theaverage Nusselt Number over a flat plate of dimension 10 cm X10 cm when air is flowing parallel to its surface with a speed 1[ms]?1.181.85X10-5 [kg.m-l.s-l], SpecificPVLCRe =V = 1 [m/s]pCpPr =Lc0.1 [m]1 1Nu = 0.664RežPr3

Numerical Exercise 1. A flat plate is supplied with a constant heat flux of 100 [W/m²] from bottom. The plate has 0.5m2 area and is kept in a room with ambient temperature 20°C. If it has a steady state temperature of 32°C what is the heat transfer coefficient? Ta = 293[K] ģ = h(T, – Ta) Tp = 305[K] %3D ģ = 100 [W /m²]

Numerical Exercise 1. A flat plate is supplied with a constant heat flux of 100 [W/m²] from bottom. The plate has 0.5m2 area and is kept in a room with ambient temperature 20°C. If it has a steady state temperature of 32°C what is the heat transfer coefficient? Ta = 293[K] ģ = h(T, – Ta) Tp = 305[K] %3D ģ = 100 [W /m²]

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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