D1=0.6m,D2=0.3m,L=3cm=0.03m,
Q=40L/s=0.04m3/s,
Q1=40l/s=0.04m3/s,Q2=80l/s=0.08m3/s
Case (i)
Flow is one dimensional and hence the velocity components v=w=0
Convective acceleration =u(∂u/∂x)
A1=4πD12=0.09πm2≈0.2827m2
A2=4πD22=0.0225πm2≈0.0707m2
u1=A1Q=0.09πm20.04m3/s≈0.1415m/s
u2=A2Q=0.0225πm20.04m3/s≈0.5657m/s
As the diameter changes uniformly, the velocity will also change uniformly. The velocity u at any distance x from inlet is given by
u=u1+Lu2–u1x
∂x∂u=Lu2−u1
Convective acceleration =u⋅Lu2−u1 x=0.015m
u=0.1415m/s+0.03m0.5657m/s–0.1415m/s⋅0.015m
=0.3536m/s
Convective acceleration
=0.3536m/s⋅0.03m0.5657m/s–0.1415m/s
=8.3355m/s2Case (ii)
Total acceleration = (convective + local ) acceleration at t =20 seconds
Rate of flow
Qt=20=Q1+40sQ2−Q1⋅20s
=0.06m3/s
u1=Q/A1=0.2122m/s
u2=Q/A2=0.8488m/s The velocity u at any distance x from inlet is given by
u=u1+Lu2–u1x
u=0.2122+21.2207x
∂x∂u=21.2207s−1Convective acceleration =u⋅∂x∂u
=(0.2122+21.2207x)⋅21.2207
At x=0.015m
(Convective acceleration )x=0.015m
=11.2578m/s2
Local acceleration
Diameter at x=0.015m is given by
D=D1+LD2–D1x=0.45m
A=4πD2≈0.1590m2
u1=Q1/A=0.2515m/s
u2=Q2/A=0.5030m/s
Rate of change of velocity
=40s0.5030m/s−0.2515m/s=0.0063m/s2
Total acceleration==11.2578m/s2+0.0063m/s2=11.2641m/s2
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