Superfly257
Industrial
- Nov 18, 2010
- 11
Hello,
I am trying to calculate the major pressure loss in my system, and I just want to make sure I've done the calculations right.
I'm not sure I'm getting entirely accurate numbers.
Just so you know, the piping is circular, and the fluid being pumped is 15W40 engine oil... the density and viscosity are based off of physical measurements of 15W40 taken in the lab.
Anyway, here are my calculations:
Givens:
½” Piping Dh=0.0127 m
10 ft of tubing = 3.048 m
Max Flow Rate (21 L/min)
Viscosity at 20°C is ? = 357.38 cSt = 0.00035738 m^2/sec
Density = 818 kg/m^3
Pipe Area= ?(0.25)^2= 0.19635 in^2
Volumetric Flow Rate=21 L/min =1281.5 in^3/min =21.36 in^3/sec
Flow Velocity=(Volumetric Flow Rate)/Area= 21.36/0.19635
=108.78 in/sec = 2.763 m/sec
Reynold's Number= (V* D_h)/? =
((2.763)(0.0127))/0.00035738 = 98.187 (Laminar)
?= 64/Re = 64/98.187 = 0.6518
Pressure Loss= ?(L/D_h )((?*V^2)/2)=0.6518(3.048/0.0127)[((818) ?(2.763)?^2)/2]= 488,439.4 Pa
I think this looks a little high, is all this correct, or did I botch it up somewhere?
Thanks,
Superfly
I am trying to calculate the major pressure loss in my system, and I just want to make sure I've done the calculations right.
I'm not sure I'm getting entirely accurate numbers.
Just so you know, the piping is circular, and the fluid being pumped is 15W40 engine oil... the density and viscosity are based off of physical measurements of 15W40 taken in the lab.
Anyway, here are my calculations:
Givens:
½” Piping Dh=0.0127 m
10 ft of tubing = 3.048 m
Max Flow Rate (21 L/min)
Viscosity at 20°C is ? = 357.38 cSt = 0.00035738 m^2/sec
Density = 818 kg/m^3
Pipe Area= ?(0.25)^2= 0.19635 in^2
Volumetric Flow Rate=21 L/min =1281.5 in^3/min =21.36 in^3/sec
Flow Velocity=(Volumetric Flow Rate)/Area= 21.36/0.19635
=108.78 in/sec = 2.763 m/sec
Reynold's Number= (V* D_h)/? =
((2.763)(0.0127))/0.00035738 = 98.187 (Laminar)
?= 64/Re = 64/98.187 = 0.6518
Pressure Loss= ?(L/D_h )((?*V^2)/2)=0.6518(3.048/0.0127)[((818) ?(2.763)?^2)/2]= 488,439.4 Pa
I think this looks a little high, is all this correct, or did I botch it up somewhere?
Thanks,
Superfly