Explanations & Calculations
- Refer to the figure attached
- Assume the flow is incompressible& non-viscous.
- ρ,d represent the densities of the oil & mercury respectively.
- Considering the central flow line & applying Bernoulli's equation for the inlet & throat sections,
P1+21ρv12P1−P2=P2+21ρv22=21ρ(v22−v12)⋯(1)
- Being incompressible, flow has a uniform rate throughout. Therefore, by considering continuity,
Q=CA1v1=CA2v2⋯ without C, the ideal volumetric flow is addressed.
- Then substituting the velocities in equation (1),
P1−P2=21ρ[C2A22Q2−C2A12Q2]=21ρC2Q2[A221−A121]⋯(2)
- By considering the hydrostatics of the Manometer: pressure at the down oil-mercury interface equals that of the same level within Mercury. Therefore,
P1+(h+x)ρgP1−P2=P2+hρg+xdg=xg(d−ρ)⋯(2)
xg(d−ρ)x=21ρC2Q2[A221−A121]=21ρC2Q2[A221−A121]×g(d−ρ)1⋯(3)
A1=π4D2=π4(30cm)2A2Qρdg=706.858cm2=176.715cm2=50×103cm3/s=800kgcm−3=13600kgcm−3=9.8×102cms−2
- Substituting these in (3),
x=2.492cm
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