Steady-state temperatures at selected nodal points ofthe symmetrical section of a flow channel are knownto be
- Determine the temperatures at nodes 1, 4, 7, and 9.
- Calculate the heat rate per unit length (W/m) fromthe outer surface A to the adjacent fluid.
- Calculate the heat rate per unit length from theinner fluid to surface B.
- Verify that your results are consistent with an overallenergy balance on the channel section.
Want to see the full answer?
Check out a sample textbook solutionChapter 4 Solutions
Introduction to Heat Transfer
- Water flows through pipe A whose diameter is 30 cm and into parallel pipes 1, 2 and 3 and out through Pipe B (diameter= 30 cm). The properties of the pipe are as follows: for pipe 1, L= 300 m, diameter = 10 cm f= 0.020; for pipe 2 L= 240 m diameter= 15 cm f= 0.018 and for pipe 3, L= 600 deiameter= 20 cm f= 0.017. The upstram junction has an Elev. 90 m with pressure of 205 kPa; the downstream junction is at Elev. 30 m. If the average velocity in pipe A is 3.0 m/s, find the flow rate in pipe 3. Provide FBD and choose the right answer below a.24.68 L/s b.212.0 L/s c.80.21 L/s d.107.11 L/s Clear my choicearrow_forwardWater flows through pipe A whose diameter is 30 cm and into parallel pipes 1, 2 and 3 and out through Pipe B (diameter= 30 cm). The properties of the pipe are as follows: for pipe 1, L= 300 m, diameter = 10 cm f= 0.020; for pipe 2 L= 240 m diameter= 15 cm f= 0.018 and for pipe 3, L= 600 deiameter= 20 cm f= 0.017. The upstram junction has an Elev. 90 m with pressure of 205 kPa; the downstream junction is at Elev. 30 m. If the average velocity in pipe A is 3.0 m/s, find the flow rate in pipe 3. include your free body diagram. a.24.68 L/s b.80.21 L/s c.107.11 L/s d.212.0 L/sarrow_forward(1) Given the working form of the Bernoulli equation as dW - F dm Where 3 is the friction heating per unit mass dP F = Au - dm Given also that friction heating in laminar flow of Newtonian fluids in circular pipes is given as -AP F =- = -gAz = Q Ax " 128 Ax is change in the x-direction. A typical capillary viscometer has a large-diameter reservoir and a long, small diameter, vertical tube. The sample is placed in the reservoir and the flow rate due to gravity is measured. The tube is 0.1 m long and has a 1 mm ID. The height of the fluid in the reservoir above the inlet to the tube is 0.02 m. The fluid being tested has a density of 1050 kg / m. The flow rate is 10* m³ / s. What is the viscosity of the fluid? Typical capillary viscometerarrow_forward
- A circuit board is cooled by passing cool helium gaş "C,= 5193 J/kg.C, v =1.233×10 m /s, p= 0.1635 kg/m Pr = 0.669, k = 0.1565 W/m.°C " through a channel [0.46 cm x14 cm×20 cm ] drilled into the board. Helium enters at 15°C and 6.8 m/s and leaves at 63.7 °C. The heat flux at the top surface of the channel can be considered to be uniform, and heat transfer through other surfaces is negligible. Assume fully developed flow for the whole channel length and (if flow is NOT Laminar use Dittus-Boelter equation:Nu=0.023 Re Pr) What is the maximum surface temperature on the circuit board (°C)? Electronic components, T, °C Не 15°C L=20 cm Channelarrow_forwardcan i get help with all parts, thanksarrow_forwardheat transferarrow_forward
- l MTN 1/1 4:26 PM 80% An oil with density 900 kg/m3 and flow rate 0.0002 m2/s flows upward through an inclined pipe as shown in figure below, The pressure at sections 1 and 2 are P1 = 350 kPa and P2 = 250 kPa, and the elevation at section 1 z1 = 0, Sections 1 and 2 are 10 m apart (L = 10 m) and the pipe is inclined at 40°. The pipe diameter is 6 cm. Assuming steady laminar flow, (a) Verify that the flow is up, (b) Compute hr between 1 and 2, (c) What is the flow rate Q, (d) Find the flow velocity, V, (e) Verify if the flow is really laminar. Flow OR directionarrow_forwardThe velocity profile for laminar flow between two plates, as in Fig.3, is 2umaxy(h-y) h4 u= If the wall temperature is Tw at both walls, use the incompressible flow energy equation to solve for the temperature distribution T (y) between the walls for steady flow. Energy equation: dT pcp dt y=h y=0 •= kV²T +4 u(y) v=W=0 Tw T(y) Fig.3. Fluid flow between two wallsarrow_forwardFluid Mechanics:arrow_forward
- Solve it correctly please. I will rate accordingly with 3votes. I need correct handwritten answer.arrow_forwardThe liquid food is flowed through an uninsulated pipe at 90 ° C. The product flow rate is 0.3 kg / s and has a density of 1000 kg / m³, specific heat 4 kJ / (kg K), a viscosity of 8 x 10-6 Pa s, and a thermal conductivity of 0.55 W / (m) K). Assume that the change in viscosity is negligible. The internal diameter of the pipe is 30 mm with a thickness of 3 mm made of stainless steel (k = 15 W / [m ° C]). The outside temperature is 15 ° C. If the outer convective heat transfer coefficient is 18 W / (m² K), calculate the heat loss at steady state per meter pipe length. a. Find the convection coefficient in pipe = W / m² ° C. b. Calculate heat loss per meter pipe length = wattsarrow_forwardThe liquid food is flowed through an uninsulated pipe at 90 ° C. The product flow rate is 0.4 kg / s and has a density of 1000 kg / m³, specific heat 4 kJ / (kg K), a viscosity of 8 x 10-6 Pa s, and a thermal conductivity of 0.55 W / (m) K). Assume that the change in viscosity is negligible. The internal diameter of the pipe is 20 mm with a thickness of 3 mm made of stainless steel (k = 15 W / [m ° C]). The outside temperature is 15 ° C. If the outer convective heat transfer coefficient is 18 W / (m² K), calculate the heat loss at steady state per meter of pipe length. a.Find the convection coefficient in the pipe = AnswerW / m² ° C. b. Calculate heat loss per meter pipe length = Answerwatt.arrow_forward
- Principles of Heat Transfer (Activate Learning wi...Mechanical EngineeringISBN:9781305387102Author:Kreith, Frank; Manglik, Raj M.Publisher:Cengage Learning