Consider pressurized liquid water flowing at m = 0. 1kg / s in a circular tube of diameter D = 0. 1m and length L = 6m . (a) If the water enters at T m , i = 500 K and the surface temperature of the tube is T s = 510 K. determine the water outlet temperature T m , o . (b) If the water enters at T m , i = 300 K and the surface temperature of the tube is T s = 310 K. determine the water outlet temperature T m , o . (c) If the water enters at T m , i = 300 K and the surface temperature of the tube is T s = 647 K. discuss whether the flow is laminar or turbulent.
Consider pressurized liquid water flowing at m = 0. 1kg / s in a circular tube of diameter D = 0. 1m and length L = 6m . (a) If the water enters at T m , i = 500 K and the surface temperature of the tube is T s = 510 K. determine the water outlet temperature T m , o . (b) If the water enters at T m , i = 300 K and the surface temperature of the tube is T s = 310 K. determine the water outlet temperature T m , o . (c) If the water enters at T m , i = 300 K and the surface temperature of the tube is T s = 647 K. discuss whether the flow is laminar or turbulent.
First monthly exam
Gas dynamics
Third stage
Q1/Water at 15° C flow through a 300 mm diameter riveted steel pipe, E-3 mm with a head loss of 6 m in
300 m length. Determine the flow rate in pipe. Use moody chart.
Q2/ Assume a car's exhaust system can be approximated as 14 ft long and 0.125 ft-diameter cast-iron pipe (
= 0.00085 ft) with the equivalent of (6) regular 90° flanged elbows (KL = 0.3) and a muffler. The
muffler acts as a resistor with a loss coefficient of KL= 8.5. Determine the pressure at the beginning of the
exhaust system (pl) if the flowrate is 0.10 cfs, and the exhaust has the same properties as air.(p = 1.74 ×
10-3 slug/ft³, u= 4.7 x 10-7 lb.s/ft²) Use moody chart
(1)
MIDAS
Kel=0.3
Q3/Liquid ammonia at -20°C is flowing through a 30 m long section of a 5 mm diameter copper tube(e =
1.5 × 10-6 m) at a rate of 0.15 kg/s. Determine the pressure drop and the head losses.
.μ= 2.36 × 10-4 kg/m.s)p = 665.1 kg/m³
2/Y
Y+1
2Cp
Q1/ Show that
Cda
Az x
P1
mactual
Cdf
Af
R/T₁
2pf(P1-P2-zxgxpf)
Q2/ A simple jet carburetor has to supply 5 Kg of air per minute. The air is at a pressure of 1.013 bar
and a temperature of 27 °C. Calculate the throat diameter of the choke for air flow velocity of 90 m/sec.
Take velocity coefficient to be 0.8. Assume isentropic flow and the flow to be compressible.
Quiz/ Determine the air-fuel ratio supplied at 5000 m altitude by a carburetor which is adjusted to give
an air-fuel ratio of 14:1 at sea level where air temperature is 27 °C and pressure is 1.013 bar. The
temperature of air decreases with altitude as given by the expression
The air pressure decreases with altitude as per relation h = 19200 log10 (1.013), where P is in bar. State
any assumptions made.
t = ts
P
0.0065h
36
2) Use the method of MEMBERS to determine the true magnitude and
direction of the forces in members1 and 2 of the frame shown below
in Fig 3.2.
300lbs/ft
member-1
member-2
30°
Fig 3.2.
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