Heat Transfer HW8a

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California State University, Fullerton *

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4123

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Aerospace Engineering

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Jan 9, 2024

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1. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt 2. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt 3. Award: 2.43 out of 2.56 points Which fluid at room temperature requires a larger pump to move at a specified velocity in a given tube? Water Castor oil Coconut oil Engine oil Engine oil requires a larger pump because of its much larger density. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt In fluid flow, which of the following is convenient to work with? V initial , T final V final , T initial V avg , T m V avg, T final In fluid flow, it is convenient to work with an average or mean velocity V avg and an average or mean temperature T m which remain constant in incompressible flow when the cross-sectional area of the tube is constant. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt The V avg and T m represent the velocity and temperature, respectively, at a cross section if all the particles were at the same velocity and different temperature. True False The V avg and T m represent the velocity and temperature, respectively, at a cross section if all the particles were at the same velocity and temperature. References True / False Difficulty: Easy Previous attempt Hints Hints
4. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt 5. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt Given are the values of Reynolds number Re of various flows. Identify the flow which is turbulent. Re = 2100 Re = 1100 Re = 3990 Re = 4010 Flow in a smooth pipe is turbulent when the Reynolds number is above 4000. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt Define hydraulic diameter. References Section Break Difficulty: Easy The hydraulic diameter is defined such that it reduces to ordinary diameter D for non-circular tubes. True False The hydraulic diameter is defined such that it reduces to ordinary diameter D for circular tubes since Nu = hD h k = 0.023Re 0.8 Pr 0.4 . Hint #1 References True / False Difficulty: Easy Previous attempt Hints Hints
6. Award: 2.43 out of 2.56 points You did not receive full credit for this question in a previous attempt 7. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt 8. Award: 2.43 out of 2.56 points You did not receive full credit for this question in a previous attempt How is hydraulic diameter defined in non-circular tubes? D h = 4 A c / p Hint #1 References Numeric Response Difficulty: Easy Previous attempt How is hydraulic diameter defined in non-circular tubes? D h = 4 A c / p Explanation: For flow-through non-circular tubes, the Reynolds number, as well as the Nusselt number and the friction factor, are based on the hydraulic diameter D h defined as D h = 4 A c / p , where A c is the cross-sectional area of the tube and p is its perimeter. Identify the fluid property responsible for the development of the velocity boundary layer and the kinds of fluids. References Section Break Difficulty: Easy What fluid property is responsible for the development of the velocity boundary layer? Viscosity of a fluid Mass density of a fluid Specific weight of a fluid Volume of a fluid The fluid viscosity is responsible for the development of the velocity boundary layer. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt For the idealized inviscid fluids, there is no velocity boundary layer . True False The fluid viscosity is responsible for the development of the velocity boundary layer. For the idealized inviscid fluids(fluids with zero viscosity), there will be no velocity boundary layer. Hint #1 References True / False Difficulty: Easy Previous attempt Hints Hints Hints
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9. Award: 2.43 out of 2.56 points You did not receive full credit for this question in a previous attempt 10. Award: 2.43 out of 2.56 points You did not receive full credit for this question in a previous attempt 11. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt Consider the fully developed region of flow in a circular tube. Identify the correct statements in this context. (Check all that apply.) The velocity profile will not change in the flow direction. The velocity profile will change in the flow direction. The temperature profile will not change in the flow direction. The temperature profile may change in the flow direction. In the fully developed region of flow in a circular tube, the velocity profile will not change in the flow direction but the temperature profile may. Hint #1 References Check All That Apply Difficulty: Easy Previous attempt Which of the following statements is true in case of the fully developed region of flow in a circular tube? The friction factor is highest at the tube inlet where the thickness of the boundary layer is zero. The friction factor decreases gradually to the fully developed value. The friction factor increases gradually to the fully developed value. The friction factor is lowest at the tube inlet where the thickness of the boundary layer is zero. The friction factor is highest at the tube inlet where the thickness of the boundary layer is zero, and decreases gradually to the fully developed value. The same is true for turbulent flow. Hint #1 References Check All That Apply Difficulty: Easy Previous attempt How does the friction factor f vary along the flow direction in the fully developed region in laminar flow and turbulent flow? The friction factor f remains constant along the flow direction in the fully developed region in both laminar and turbulent flow. The friction factor f varies along the flow direction in the fully developed region in both laminar and turbulent flow. The friction factor f remains constant along the flow direction in the fully developed region in laminar flow and varies in turbulent flow. The friction factor f varies along the flow direction in the fully developed region in laminar flow and remains constant in turbulent flow. The friction factor f remains constant along the flow direction in the fully developed region in both laminar and turbulent flow. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt Hints Hints Hints
12. Award: 2.43 out of 2.56 points You did not receive full credit for this question in a previous attempt 13. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt Identify the correct statements in the context of friction factors of laminar and turbulent flows. (Check all that apply.) In turbulent flow, the tubes with rough surfaces have much higher friction factors than the tubes with smooth surfaces. In turbulent flow, the tubes with rough surfaces have much lower friction factors than the tubes with smooth surfaces. In laminar flow, the friction factor is dependent on the surface roughness. In laminar flow, the friction factor is independent of the surface roughness. In turbulent flow, the tubes with rough surfaces have much higher friction factors than the tubes with smooth surfaces. In the case of laminar flow, the effect of surface roughness on the friction factor is negligible. Hint #1 References Check All That Apply Difficulty: Easy Previous attempt Identify the correct expression for hydrodynamic entry length L h for Reynolds number = 20, given that D is the tube diameter. L h = 1.3 D L h = D L h = 1.6 D L h =1.4 D L h = 0.05 × Re × D = 0.05 × 20 × D = 1 D Hint #1 References Multiple Choice Difficulty: Easy Previous attempt Hints Hints
14. Award: 2.43 out of 2.56 points L h = 0.05Re D L t = 0.05RePr D L t 10 D L h 10 D You received credit for this question in a previous attempt 15. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt Match the turbulent and laminar flows (in the left column) to their hydrodynamic and thermal entry lenghts (in the right column). 1. Thermal entry length of laminar flow 2. Hydrodynamic length of turbulent flow 3. Hydrodynamic entry length of laminar flow 4. Thermal entry length of turbulent flow The hydrodynamic and thermal entry lengths are given as L h = 0.05Re D and L t = 0.05RePr D for laminar flow, and L h L t 10 D in turbulent flow. Noting that Pr >> 1 for oils, the thermal entry length is larger than the hydrodynamic entry length in laminar flow. In turbulent, the hydrodynamic and thermal entry lengths are independent of Re or Pr numbers, and are comparable in magnitude. Hint #1 References Matching Difficulty: Easy Previous attempt Which of the following statements are true for laminar and turbulent flows? (Check all that apply.) Pr >> 1 for oils, the thermal entry length is larger than the hydrodynamic entry length in laminar flow. Pr << 1 for oils, the hydrodynamic entry length is larger than the thermal entry length in laminar flow. Pr << 1 for liquid metals, the thermal entry length is smaller than the hydrodynamic entry length in laminar flow. Pr << 1 for liquid metals, the hydrodynamic entry length is smaller than the thermal entry length in laminar flow. In turbulent, the hydrodynamic and thermal entry lengths are independent of Re or Pr numbers, and are comparable in magnitude. In turbulent, the hydrodynamic and thermal entry lengths are dependent of Re or Pr numbers, and are not comparable in magnitude. Pr >> 1 for oils, the thermal entry length is larger than the hydrodynamic entry length in laminar flow. Pr << 1 for liquid metals, the thermal entry length is smaller than the hydrodynamic entry length in laminar flow. In turbulent, the hydrodynamic and thermal entry lengths are independent of Re or Pr numbers and are comparable in magnitude. Hint #1 References Check All That Apply Difficulty: Easy Previous attempt Correct: 3 3 Correct: 1 1 Correct: 4 4 Correct: 2 2 Hints Hints
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16. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt 17. Award: 2.43 out of 2.56 points You did not receive full credit for this question in a previous attempt 18. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt The region in which the flow is both hydrodynamically and thermally developed is called the _____ region. hydro-thermal entrance fully developed boundary layer irrotational flow The region in which the flow is both hydrodynamically (the velocity profile is fully developed and remains unchanged) and thermally (the dimensionless temperature profile remains unchanged) developed is called the fully developed region. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt Consider laminar forced convection in a circular tube. The heat transfer coefficient is highest _____. at the outlet of the tube at a distance one-fourth of the length of the tube from the tube inlet at the mid of the tube at the inlet of the tube The heat transfer coefficient is highest at the tube inlet where the thickness of thermal boundary layer is zero. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt For turbulent forced convection in a circular tube, the heat flux will be higher near the inlet because the heat transfer coefficient is highest at the tube inlet where the thickness of thermal boundary layer is zero, and decreases gradually to the fully developed value. True False For turbulent forced convection in a circular tube, the heat flux will be higher near the inlet because the heat transfer coefficient is highest at the tube inlet where the thickness of thermal boundary layer is zero, and decreases gradually to the fully developed value. Hint #1 References True / False Difficulty: Easy Previous attempt Hints Hints Hints
19. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt 20. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt 21. Award: 2.43 out of 2.56 points You did not receive full credit for this question in a previous attempt 22. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt Which of the following is an exact representation of the average temperature difference between the fluid and the surface for an entire tube? T ln T e T m T diff The logarithmic mean temperature difference T ln is an exact representation of the average temperature difference between the fluid and the surface for an entire tube. It truly reflects the exponential decay of the local temperature difference. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt Consider fluid flow in a tube whose surface temperature remains constant. Identify the appropriate temperature difference for use in Newton’s law of cooling with an average heat transfer coefficient. T lm = ( T e T i )/ ln( T e / T i ) T lm = ln( T e T i )/ ( T e / T i ) T lm = ( T e T i )/ ln( T i T e ) T lm = ln( T e T i )/ ( T i T e ) When the surface temperature of a tube is constant, the appropriate temperature difference for use in the Newton's law of cooling is the logarithmic mean temperature difference that can be expressed as T lm = ( T e T i )/ ln( T e / T i ) Hint #1 References Multiple Choice Difficulty: Easy Previous attempt What do small and large NTU values tell about a heat transfer system? A small value of NTU (NTU < 5) indicates that heat transfer will not increase no matter how much we extend the length of a tube, whereas a large NTU value (NTU > 5) indicates more opportunities for heat transfer. A small value of NTU (NTU < 10) indicates that heat transfer will not increase no matter how much we extend the length of a tube, whereas a large NTU value (NTU >10) indicates more opportunities for heat transfer. A small value of NTU (NTU < 10) indicates more opportunities for heat transfer, whereas a large NTU value (NTU > 10) indicates that heat transfer will not increase no matter how much we extend the length of a tube. A small value of NTU (NTU < 5) indicates more opportunities for heat transfer, whereas a large NTU value (NTU > 5) indicates that heat transfer will not increase no matter how much we extend the length of a tube. The number of transfer units NTU is a measure of the heat transfer area and effectiveness of a heat transfer system. A small value of NTU (NTU < 5) indicates more opportunities for heat transfer, whereas a large NTU value (NTU >5) indicates that heat transfer will not increase no matter how much we extend the length of a tube. Hint #1 References Multiple Choice Difficulty: Easy Previous attempt Hints Hints Hints
Air enters an 18-cm-diameter, 12-m-long underwater duct at 50°C and 1 atm at a mean velocity of 7 m/s and is cooled by the water outside. If the average heat transfer coefficient is 65 W/ m 2 · K and the tube temperature is nearly equal to the water temperature of 7°C, determine the exit temperature of air and the rate of heat transfer. The properties of air at a bulk mean temperature of 30°C are ρ = 1.164 kg/m 3 and c p = 1007 J/kg·°C. Is this a good assumption? The exit temperature of air is 12.18 °C. The rate of heat transfer is 7.88 kW. 30°C is an appropriate temperature to evaluate the fluid properties. Hint #1 References Multi-Answer Difficulty: Medium Previous attempt Air enters an 18-cm-diameter, 12-m-long underwater duct at 50°C and 1 atm at a mean velocity of 7 m/s and is cooled by the water outside. If the average heat transfer coefficient is 65 W/ m 2 · K and the tube temperature is nearly equal to the water temperature of 7°C, determine the exit temperature of air and the rate of heat transfer. The properties of air at a bulk mean temperature of 30°C are ρ = 1.164 kg/m 3 and c p = 1007 J/kg·°C. Is this a good assumption? The exit temperature of air is 12.1976 ± 2% °C. The rate of heat transfer is 7.8913 ± 2% kW. 30°C is an appropriate temperature to evaluate the fluid properties. Explanation: The following assumptions have been made here: 1. Steady operating conditions exist. 2. The surface temperature of the duct is constant. 3. The thermal resistance of the duct is negligible. The mass flow rate of water is ˙ m = ρA c V avg = ρ π D 2 4 V avg ˙ m = 1.164 kg/m 3 π 0.18 m) 2 4 (7 m/s) ˙ m = 0.2073 kg/s A s = π DL = π 0.18 m) 12 m A s = 6.786 m 2 The exit temperature of air is determined from T e = T s T s T i e hA s ˙ mc p T e = 7 − 7 − 50 e (65 ) (6.786) (0.2073) (1007 ) T e = 12.1976°C The logarithmic mean temperature difference and the rate of heat transfer are ΔT lm = T e T i ln T s T e T s T i ΔT lm = 12.1976 −50 ln 7 −12.1976 7−50 ΔT lm = 17.8904°C ˙ Q = hA s ΔT lm ˙ Q = 65 W/m 2 ·°C 6.786 m 2 (17.8904°C) ˙ Q = 7.8913 kW The bulk mean temperature here is ( 12.1976 +50 ) °C 2 = 31.1°C. This is close to 30ºC. Hence, the assumption made here is correct. ( ) ( ) ( ( ( ) ( ) ( ) ( ) ( ) ( ) ( )( ) Hints
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23. Award: 2.43 out of 2.56 points You received credit for this question in a previous attempt 24. Award: 2.43 out of 2.56 points You did not receive full credit for this question in a previous attempt Which of the following is used to determine the volume flow rate in a circular pipe with laminar flow? . V = V avg /2 A c . V = V avg A c = V max /2 A c . V = 4 V max 3 . V = 3 V max 4 The volume flow rate in a circular pipe with laminar flow can be determined by measuring the velocity at the centerline in the fully developed region, multiplying it by the cross-sectional area, and dividing the result by 2 since . V = V avg A c = V max /2 A c Hint #1 References Multiple Choice Difficulty: Easy Previous attempt The average velocity in a circular pipe in fully developed laminar flow can be determined by simply measuring the velocity at R /2. True False The average velocity in a circular pipe in fully developed laminar flow cannot be determined by simply measuring the velocity at R /2 (midway between the wall surface and the centerline). The mean velocity is V max /2, but the velocity at R /2 is V R /2 = V max 1 r 2 R 2 r = R / 2 = 3 V max / 4 References True / False Difficulty: Easy Previous attempt ( ) ( ) ( ) ( ) ( ) Hints