The core of a high-temperature, gas-cooled nuclear reactor has coolant tubes of 20-mm diameter and 780-mm length. Helium enters at 600 K and exits at 1000 K when the flow rate is 8 × 10 − 3 kg / s per tube. (a) Determine the uniform tube wall surface temperature for these conditions. (b) If the coolant gas is air, determine the required how rate if the heat removal rate and tube wall surface temperature remain the same. What is the outlet temperature of the air?
The core of a high-temperature, gas-cooled nuclear reactor has coolant tubes of 20-mm diameter and 780-mm length. Helium enters at 600 K and exits at 1000 K when the flow rate is 8 × 10 − 3 kg / s per tube. (a) Determine the uniform tube wall surface temperature for these conditions. (b) If the coolant gas is air, determine the required how rate if the heat removal rate and tube wall surface temperature remain the same. What is the outlet temperature of the air?
Solution Summary: The author explains the surface temperature of helium, the mass flow rate, and the Reynolds number for the type of flow.
The core of a high-temperature, gas-cooled nuclear reactor has coolant tubes of
20-mm
diameter and 780-mm length. Helium enters at 600 K and exits at 1000 K when the flow rate is
8
×
10
−
3
kg
/
s
per tube.
(a) Determine the uniform tube wall surface temperature for these conditions.
(b) If the coolant gas is air, determine the required how rate if the heat removal rate and tube wall surface temperature remain the same. What is the outlet temperature of the air?
5. Steam condensing on the outer surface of a thin-walled circular tube of 50 mm diameter and 6 m
length maintains a uniform surface temperature of 100 C. Water flows through the tube at a rate of
m= 0.25 kg/s, and its inlet and outlet temperatures are Tmi = 15 C and Tmo = 57C. What is the
average convection coefficient associated with the water flow?
Data: Pvater = 1000 kg/m³ ; c, = 4.2 kJ/kg-K.
Consider pressurized water, engine oil (unused), and Nak (22%/78%) flowing in a 20-mm-diameter tube.
(a) Determine the mean velocity, in m/s, the hydrodynamic entry length, in m, and the thermal entry length, in m, for each of the fluids
when the fluid temperature is 366 K and the flow rate is 0.01 kg/s.
(b) Determine the mass flow rate, in kg/s, the hydrodynamic entry length, in m, and the thermal entry length, in m, for water and engine
oil at 300 and 400 K and a mean velocity of 0.022 m/s.
Part A
Determine the mean velocity, in m/s, the hydrodynamic entry length, in m, and the thermal entry length, in m, for each of the fluids
when the fluid temperature is 366K and the flow rate is 0.01 kg/s.
Liquid
Um (m/s)
Xfdh (m)
Xfd,t (m)
water
i
engine oil
i
i
i
Nak
i
Current Attempt in Progress
Consider pressurized water, engine oil (unused), and Nak (22 %/78%) flowing in a 20-mm-diameter tube.
(a) Determine the mean velocity, in m/s, the hydrodynamic entry length, in m, and the thermal entry length, in m, for each of the fluids
when the fluid temperature is 366 K and the flow rate is 0.014 kg/s.
(b) Determine the mass flow rate, in kg/s, the hydrodynamic entry length, in m, and the thermal entry length, in m, for water and engine
oil at 300 and 400 K and a mean velocity of 0.018 m/s.
Part A
Your answer is incorrect.
Determine the mean velocity, in m/s, the hydrodynamic entry length, in m, and the thermal entry length, in m, for each of the fluids
when the fluid temperature is 366 K and the flow rate is 0.014 kg/s.
Liquid
water
engine oil
Nak
(m/s)
!
i
XALA(M)
xer (m)
Attempts: unlimited Submit Answer
Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering)
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