Heat Transfer
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Heat Transfer Please be neat and organized for a thumbs up! Problem 3 Atmospheric air at...
Clear solutions please fully worked out for a thumbs up, thanks! . Compare the external flows of two different fluids over a flat plate held at a constant T,; air at a free-stream speed Ux-3 m and temperature Too-250 K to that of engine oil at a free-stream speed Un-3 ! ! and temperature T 400 K. For laminar flow over a flat plate, the velocity boundary layer thickness is given by δ- (In the absence of a known surface...
Exercise 2 Air at 20 °C and 1 atm flows over a flat plate at 50 m/s. The plate is 300 cm long and is maintained at 60C. The width of the plate is 2 m. The critical Rec = 5 x 105 The properties are Conductivity k = 0.0263 W/mK, kinematic viscosity nu = v = 15.89 x 10-6 m²/s, Prandtl number is Pr=0.707 Density rho = p = 1.128 kg/m3 1. Determine the critical length Xc 2. Determine...
Air at T=25°C and pressure P=1 bar flows over a square plate with a velocity V=1 m/s. This plate has a length L= 1 m and it is heated over its entire length; the plate temperature is constant Tp=100°C. The following data are given. For air: dynamic viscosity: mu = 1.9*10–5 kg/(m.s); density: rho = 1.05 kg/m3; conductivity k = 0.03 W/(m K); Specific heat Cp = 1.007 kJ/(kg K); Prandtl number Pr = 0.7 For laminar flow over a...
Problem 1: Air at 100 degrees Celsius, 1 atm and a free stream velocity of 5 m/s flows over a 3 meter long, thin, flat plate of naphthalene, causing it to sublime... Please answer all parts Problem 1. (20 Points) Air at 100°C, 1 atm, and a free-stream velocity of 5 m/s flows over a 3- m-long, thin, flat plate of naphthalene, causing it to sublime. (a) Determine the length over which a laminar boundary layer persists. (b) For that...
Use the integral method for boundary layer flow and convective heat transfer over a flat plate heated by maintaining a constant heat flux q"w, for the case of very low Prandtl number, Pr0. Assume that the free stream velocity of the fluid, U, and free stream temperature, T-do not vary with x. Using the integral form of energy equation, show that under these conditions: (a) the temperature profile, (T- T) is given by, 41 2 CT-T oa (b) the wall...
Consider air flows with velocity of U?=U= 10 m/s over a semi-finite smooth flat plate with L=97 cm long. Calculate the followings by assuming ? = 1.568 x 10-5 m2/s and ?=1.177 kg/m3. Figure 1 : Boundary layer over a flat plate Consider air flows with velocity of U?=U=10 m/s over a semi-finite smooth flat plate with L=97 cm long. Calculate the followings by assuming ? = 1.568 x 10-5 m2/s and ?=1.177 kg/m3. b) Under some flow and boundary...
Please, I need the answer for this problem as soon as possible with all the steps thanks USE EES Air Flows over over a flat metal plate at a velocity of 10 m/s. The 3 (а) plate is 0.7 m long and at a temperature of 315 °C. What is the rate of heat transfer required to maintain the plate at 28°C. Assume flow is laminar over the ENTIRE wwwww PLATE 3(b) boundary layer thickness Now calculate the (i) the...
Problem 1: In an experiment, Mercury at film temperature of 127 C flows over a flat plate of length 500 mm and width of 20 mm. Results reveal that the velocity boundary layer thickness at the distance of 5 mm from the leading edge is 0.4 pim, and also th convection heat transfer coefficients in the laminar and turbulent regions (Rex.-2 x 10) take the form of GX İsit where x is measured in meters from the leading edge of...
Question 1 25 ترفع الاجابة على شكل ملف PDF يحوي جميع الأجوية 1: Atmospheric air at 25°C flows with a velocity of 40 m/s past a flat plate 0.75 m long and 0.4 m wide. The surface of the plate is maintained at 275°C. Estimate: (a) the total heat transferred and the total drag force on one side of the plate (b) fraction of the heat transfer and drag force for laminar portion of flow (c) what error in part...
(2 pts) Heat is transferred from a hot fluid (temperature T1 and heat transfer coefficient h2) through a plane wall of thickness 8, surface area A and the thermal conductivity k. The thermal resistance for the set up is + (a) AC ) (b) A (i + + ) (c) 2 (na + + n2) (d) A (na + b +h2) (2 pts) An increase in convective heat transfer coefficient over a fin will (a) increase effectiveness (b) decrease effectiveness...