steam flow range calculation

Hi,

I am sam from chennai. This will b useful for u, i think...........

As long as the fluid speed is sufficiently subsonic (V < mach 0.3), the incompressible Bernoulli's equation describes the flow reasonably well. Applying this equation to a streamline traveling down the axis of the horizontal tube gives,

where location 1 is upstream of the orifice, and location 2 is slightly behind the orifice. It is recommended that location 1 be positioned one pipe diameter upstream of the orifice, and location 2 be positioned one-half pipe diameter downstream of the orifice. Since the pressure at 1 will be higher than the pressure at 2 (for flow moving from 1 to 2), the pressure difference as defined will be a positive quantity.

From continuity, the velocities can be replaced by cross-sectional areas of the flow and the volumetric flowrate Q,

Solving for the volumetric flowrate Q gives,

The above equation applies only to perfectly laminar, inviscid flows. For real flows (such as water or air), viscosity and turbulence are present and act to convert kinetic flow energy into heat. To account for this effect, a discharge coefficient C_d is introduced into the above equation to marginally reduce the flowrate Q,

Since the actual flow profile at location 2 downstream of the orifice is quite complex, thereby making the effective value of A₂ uncertain, the following substitution introducing a flow coefficient C_f is made,

where A_o is the area of the orifice. As a result, the volumetric flowrate Q for real flows is given by the equation,

The flow coefficient C_f is found from experiments and is tabulated in reference books; it ranges from 0.6 to 0.9 for most orifices. Since it depends on the orifice and pipe diameters (as well as the Reynolds Number), one will often find C_f tabulated versus the ratio of orifice diameter to inlet diameter, sometimes defined as b,

The mass flowrate can be found by multiplying Q with the fluid density,

Thank you sir .very nice explanation . i am instrumentation engineer . i am having this doubt from long time. thank you once again.

Me too. Thank you Sir.

Dear Guest,

I think that you made an error when you state that the flow ha to be "laminar" for the validity of the equation.

If the flow is laminar the velocity is not constant over the section but varies in a parabolic way so that the equations are totally different AND by the calculation the dynamic viscosity of the fluid has to be considered.

I would suggest since you did such a good job you look once more and make yourself the corrections.