Air at 20 °C and 1 atm. flow over a flat plate with 35 m/s. The...
Air at 20 °C and 1 atm. flow over a flat plate with 35 m/s. The size of the plate is 75 cm by 75 cm and is maintained at 60 °C. Calculate:
a) The heat transfer rate 40 cm from the leading edge of the plate.
b) The heat transfer rate at the end of the plate (at x = L).
c) The heat transfer rate from the entire plate.
d) The heat transfer rate at the end of the hot plate if it is preceded by unheated section of 25 cm.
please first schematic and assumption
using the book incoropera
Homework Answers
Required information Air at 25°C and 1 atm is flowing over a long flat plate with...
Required information Air at 25°C and 1 atm is flowing over a long flat plate with a velocity of 7 m/s. The density and kinematic viscosity of air at 1 atm and 25°C are p= 1.184 kg/m3 and V = 1.562x10-5 m2/s. Calculate the distance from the leading edge of the plate where the flow becomes turbulent. The distance from the leading edge of the plate is m. Required information Air at 25°C and 1 atm is flowing over a...
8) Air flows over a flat plate at a velocity of 20 m/s and a temperature...
8) Air flows over a flat plate at a velocity of 20 m/s and a temperature of 20C. The surface temperature of the plate is 134C, and the length of the plate in the direction of flow is 1.5 m. Properties of air may be taken as A-0.030 W/m-C, Pr-0.700, and a/p 2.092E-5 m/s (5% ) What is the location from the leading edge, X, where the flow becomes turbulent Re (20)15 a l Ve30s T20 T LaLS 523 m...
2. A heated flat plate 1.0 m long (in the direction of flow) and 0.5 m...
2. A heated flat plate 1.0 m long (in the direction of flow) and 0.5 m wide is maintained at a constant temperature of 100°C. Cooling water at a temperature of 24°C flows over the top of the plate at 15 cm/s. Assume the bottom of the plate is adiabatic. a. Determine the heat transfer rate from the plate. b. A trip wire is placed at the leading edge of the plate, tripping the flow to turbulent. Determine the heat...
Air at a temperature of 300 K flows over one side of a flat plate of...
Air at a temperature of 300 K flows over one side of a flat plate of width 1 m at a velocity of 20 m/s. The plate has a constant surface temperature of 350 K. Assume Re(x,c)=5x10^5. a) What is the velocity boundary layer thickness at the end of the plate if L=0.25 m? What if L=1 m? b) Calculate the drag on the plate if L=0.25 m. What is the drag if L=1 m? c) Find the heat transfer...
Air at 25 °C and 1 atm is flowing over a long flat plate with a...
Air at 25 °C and 1 atm is flowing over a long flat plate with a velocity of 8 m/s. (a) Determine the distance from the leading edge of the plate where the flow becomes turbulent. (b) What will be the boundary layer thickness at the end of the plate? (c) If the plate is a 2m by 2 m square, what will be the friction drag acting on the plate? Schematic Given ssumptions Find v=8m/s xcr ,FD ,δ@x=L L-2m...
Exercise 2 Air at 20 °C and 1 atm flows over a flat plate at 50...
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...
Hot carbon dioxide exhaust gas at 1 atm is being cooled by flat plates. The gas...
Hot carbon dioxide exhaust gas at 1 atm is being cooled by flat
plates. The gas at 220°C flows in parallel over the upper and lower
surfaces of a 1.4-m-long flat plate at a velocity of 1.8 m/s and
the flat plate surface temperature is maintained at 80°C. The
properties of CO2 at Tf = (220°C + 80°C)/2 = 150°C are k = 0.02652
W/m∙K, ν = 1.627 × 10−5 m2/s, and Pr = 0.7445. Determine the local
convection heat...
Air at a pressure of 1 atm and a temperature of 60 °C is in parallel...
Air at a pressure of 1 atm and a temperature of 60 °C is in parallel flow over the top surface of a flat plate that is heated to a uniform temperature of 194 °C. The plate has a length of 0.30 m (in the flow direction) and a width of 0.20 m. The Reynolds number based on the plate length is 60,000. 1) Draw an annotated schematic of the problem. 2) What is the rate of heat transfer from...
1. For laminar flow over a flat plate, the local heat transfer coefficient, hx, is known to vary as hx~Cx-12 where C is...
1. For laminar flow over a flat plate, the local heat transfer coefficient, hx, is known to vary as hx~Cx-12 where C is a constant and x is the distance from the leading edge (x-0) of the plate. What is the ratio of the average coefficient between the leading edge and some location x on the plate (h,) to the local coefficient at x (h)? (15%)
1. For laminar flow over a flat plate, the local heat transfer coefficient, hx,...
For laminar flow over a flat plate, the local heat transfer coefficient hx =x-1/2 where x...
For laminar flow over a flat plate, the local heat transfer coefficient hx =x-1/2 where x is the distance from the leading edge (x-0) of the plate. What is the average heat transfer coefficient from the leading edge to location x
Required information Air at 25°C and 1 atm is flowing over a long flat plate with a velocity of 7 m/s. The density and kinematic viscosity of air at 1 atm and 25°C are p= 1.184 kg/m3 and V = 1.562x10-5 m2/s. Calculate the distance from the leading edge of the plate where the flow becomes turbulent. The distance from the leading edge of the plate is m. Required information Air at 25°C and 1 atm is flowing over a...
8) Air flows over a flat plate at a velocity of 20 m/s and a temperature of 20C. The surface temperature of the plate is 134C, and the length of the plate in the direction of flow is 1.5 m. Properties of air may be taken as A-0.030 W/m-C, Pr-0.700, and a/p 2.092E-5 m/s (5% ) What is the location from the leading edge, X, where the flow becomes turbulent Re (20)15 a l Ve30s T20 T LaLS 523 m...
2. A heated flat plate 1.0 m long (in the direction of flow) and 0.5 m wide is maintained at a constant temperature of 100°C. Cooling water at a temperature of 24°C flows over the top of the plate at 15 cm/s. Assume the bottom of the plate is adiabatic. a. Determine the heat transfer rate from the plate. b. A trip wire is placed at the leading edge of the plate, tripping the flow to turbulent. Determine the heat...
Air at 25 °C and 1 atm is flowing over a long flat plate with a velocity of 8 m/s. (a) Determine the distance from the leading edge of the plate where the flow becomes turbulent. (b) What will be the boundary layer thickness at the end of the plate? (c) If the plate is a 2m by 2 m square, what will be the friction drag acting on the plate? Schematic Given ssumptions Find v=8m/s xcr ,FD ,δ@x=L L-2m...
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...
Hot carbon dioxide exhaust gas at 1 atm is being cooled by flat
plates. The gas at 220°C flows in parallel over the upper and lower
surfaces of a 1.4-m-long flat plate at a velocity of 1.8 m/s and
the flat plate surface temperature is maintained at 80°C. The
properties of CO2 at Tf = (220°C + 80°C)/2 = 150°C are k = 0.02652
W/m∙K, ν = 1.627 × 10−5 m2/s, and Pr = 0.7445. Determine the local
convection heat...
Air at a pressure of 1 atm and a temperature of 60 °C is in parallel flow over the top surface of a flat plate that is heated to a uniform temperature of 194 °C. The plate has a length of 0.30 m (in the flow direction) and a width of 0.20 m. The Reynolds number based on the plate length is 60,000. 1) Draw an annotated schematic of the problem. 2) What is the rate of heat transfer from...
1. For laminar flow over a flat plate, the local heat transfer coefficient, hx, is known to vary as hx~Cx-12 where C is a constant and x is the distance from the leading edge (x-0) of the plate. What is the ratio of the average coefficient between the leading edge and some location x on the plate (h,) to the local coefficient at x (h)? (15%)
1. For laminar flow over a flat plate, the local heat transfer coefficient, hx,...
For laminar flow over a flat plate, the local heat transfer coefficient hx =x-1/2 where x is the distance from the leading edge (x-0) of the plate. What is the average heat transfer coefficient from the leading edge to location x
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