"D_1=0.6m, D_2=0.3m,L=3cm=0.03m,"
"Q=40L\/s=0.04m^3\/s,"
"Q_1=40l\/s=0.04m^3\/s,Q_2=80l\/s=0.08m^3\/s"
Case (i)
Flow is one dimensional and hence the velocity components "v=w=0"
Convective acceleration "=u(\\partial u\/\\partial x)"
"A_1=\\dfrac{\\pi D_1^2}{4}=0.09\\pi m^2\\approx0.2827m^2"
"A_2=\\dfrac{\\pi D_2^2}{4}=0.0225\\pi m^2\\approx0.0707m^2"
"u_1=\\dfrac{Q}{A_1}=\\dfrac{0.04m^3\/s}{0.09\\pi m^2}\\approx0.1415m\/s"
"u_2=\\dfrac{Q}{A_2}=\\dfrac{0.04m^3\/s}{0.0225\\pi m^2}\\approx0.5657m\/s"
As the diameter changes uniformly, the velocity will also change uniformly. The velocity "u" at any distance "x" from inlet is given by
"\\text{Convective acceleration }=u\\cdot \\dfrac{u_2-u_1}{L}"
"x=0.015m"
"=0.3536m\/s"
"\\text{Convective acceleration }"
"=8.3355m\/s^2"
Case (ii)
Total acceleration = (convective + local ) acceleration at t =20 seconds
Rate of flow
"Q_{t=20}=Q_1+\\dfrac{Q_2-Q_1}{40s}\\cdot20s""=0.06m^3\/s"
"u_1=Q\/A_1=0.2122m\/s"
"u_2=Q\/A_2=0.8488m\/s"
The velocity "u" at any distance "x" from inlet is given by
"u = 0.2122 +21.2207 x"
"\\dfrac{\\partial u}{\\partial x}=21.2207s^{-1}""\\text{Convective acceleration }=u\\cdot \\dfrac{\\partial u}{\\partial x}"
"=(0.2122 +21.2207 x)\\cdot21.2207"
At "x=0.015m"
"=11.2578m\/s^2"
Local acceleration
Diameter at "x=0.015m" is given by
"A=\\dfrac{\\pi D^2}{4}\\approx0.1590m^2"
"u_2=Q_2\/A=0.5030m\/s"
"\\text{Rate of change of velocity}"
"=\\dfrac{0.5030m\/s-0.2515m\/s}{40s}=0.0063m\/s^2"
Total acceleration="=11.2578m\/s^2+0.0063m\/s^2=11.2641m\/s^2"
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