Flow in valves and fittings

orifice, Venturi tube, nozzle flow

pipe flow calculator

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Resistance coefficient K, valves and fittings head loss and flow velocity | Pipe equivalent length L/D

Pressure drop or head loss is proportional to the velocity in valves or fittings. For the most engineering practices it can be assumed that pressure drop or head loss due to flow of fluids in turbulent range through valves and fittings is proportional to square of velocity.

To avoid expensive testing of every valves and every fittings that are installed on pipeline, the experimental data are used. For that purpose resistance coefficient K, equivalent length L/D and flow coefficient Cv, Kv are used. These values are available from different sources like tables and diagrams from different authors and from valves manufacturers as well.

Kinetic energy, which is represented as head due to velocity is generated from static head and increase or decrease in velocity directly is proportional with static head loss or gain. "Velocity head" is:

velocity head

where is: hL - head loss; v - velocity; gn - acceleration of gravity;

The number of velocity heads lost due to resistance of valves and fittings is:

velocity head loss in valves and fittings

where is: hL - head loss; K - resistance coefficient; v - velocity; gn - acceleration of gravity;

Resistance coefficient K calculator

Resistance factor K calculation for elbows, bends, tees, pipe entrance, pipe exit, pipe reducers, pipe enlargement.

The head loss due to resistance in valves and fittings are always associated with the diameter on which velocity occurs.

The resistance coefficient K is considered to be constant for any defined valves or fittings in all flow conditions, as the head loss due to friction is minor compared to the head loss due to change in direction of flow, obstructions and sudden or gradual changes in cross section and shape of flow.

Head loss due to friction in straight pipe is expressed by the Darcy equation:

velocity head loss in pipe

where is: hL - head loss; f - friction factor; L - length; D - internal diameter; v - velocity; gn - acceleration of gravity;

It follows that:

equivalent length

where is: K - resistance coefficient; f - friction factor; L - length; D - internal diameter;

The ratio L/D is equivalent length in pipe diameters of straight pipe that will cause the same pressure drop or head loss as the valves or fittings under the same flow conditions. As the resistance coefficient is K is constant the equivalent length L/D will vary inversely with the change in friction factor for different flow conditions.

For geometrically similar valves and fittings, the resistance coefficient would be constant. Actually there are always smaller or bigger geometrical non similarity in valves and fittings of different nominal size, so the resistance coefficient is not constant. The resistance coefficient K for a given type of valves or fittings, tends to vary with size as does friction factor for straight clean commercial steel pipe at the same flow conditions.

Some resistances in piping like sudden or gradual contractions and enlargements, as well as pipe entrances or exists are geometrically similar. Therefore the resistance coefficient or equivalent length L/D is for these items independent of size.

The values for resistance coefficient or equivalent length L/D are always associated with internal pipe diameter where the resistance is occurring.

If the resistance coefficient or equivalent length L/D should be used for different internal pipe diameter than the diameter for which existing values can be found following relationship can be used:

equivalent diameter

where is: K - resistance coefficient; D - internal diameter;

where subscript "a" defines K and d with the reference to internal pipe diameter, and subscript "b" defines K and d with the reference to the internal diameter for which values of K can be found in tables or diagrams.

This equation can also be used if the piping system has more than one size of valves and fittings to express the resistance coefficient or equivalent length L/D in terms of one size.

Resistance coefficient K for internal diameter sudden and gradual contraction and enlargement

Using momentum, continuity and Bernoulli equation the resistance due to sudden enlargements may be expressed as:

sudden enlargement resistance coefficient

and the resistance factor due to sudden contraction as:

sudden contraction resistance coefficient

where is: K1 - resistance coefficient; d1 - internal diameter (smaller); d2 - internal diameter (larger);

Using β as diameter ratio, both equation can be expressed as:

resistance coefficient

where is: K1 - resistance coefficient; β - diameter ratio d1/d2;

In order to express the resistance coefficient in terms of larger pipe diameter, following relation should be used:

resistance coefficient

where is: K1 - resistance coefficient based on smaller internal diameter; K2 - resistance coefficient based on larger internal diameter; β - diameter ratio d1/d2;

If the enlargement is not sudden but gradual, or if angle of gradual enlargement is different from 180O, Gibson coefficient Ce can be used for different angle of divergence as follows:

Gibson coefficient Gibson coefficient

In other words, if angle of divergence is bigger than 45O, the resistance coefficient is equal to one for sudden enlargement.

For gradual contraction the resistance coefficient on the same basis based on Crane test data, contraction coefficient Cc can be used for different angles of convergence, as follows:

gradual contraction resistance coefficient gradual contraction resistance coefficient

Using above expressions for enlargement and contraction coefficient, resistance coefficient can be calculated as:

For gradual enlargement:

resistance ceofficient gradual enlargement resistance ceofficient gradual enlargement

where is: Ce - coefficient of enlargement; K1 - resistance coefficient based on smaller internal diameter; β - diameter ratio d1/d2; θ - enlargement angle;

For gradual contraction:

resistance ceofficient gradual contraction

resistance ceofficient gradual contraction

where is:

Cc - coefficient of contraction; K1 - resistance coefficient based on smaller internal diameter; β - diameter ratio d1/d2; θ - enlargement angle;

For resistance coefficient based on the large pipe diameter expression:

resistance ceofficientbased on large diameter

should be used, with above equations.

where is: K1 - resistance coefficient based on smaller internal diameter; K2 - resistance coefficient based on larger internal diameter; β - diameter ratio d1/d2;

Equations for gradual enlargement and contraction can be used for resistance coefficient calculation for reduced bore straight-through valves like ball valves and gate valves. The total resistance coefficient for this type of ball and gate valves is the summation of resistance coefficient for gradual contraction and gradual enlargement.

You can calculate resistance coefficient using resistance coefficient K and equivalent length l/d calculator.

Flow coefficient Cv, pressure drop, control valve flow rate

Flow coefficient Cv calculator

Calculate flow coefficient Cv or Kv for known flow capacity and pressure difference. Calculate maximum flow capacity of control valve for known flow coefficient Cv or Kv and pressure difference. Calculate pressure difference for known flow coefficient Cv or Kv and flow capacity.

Selecting the correct valve size for a given application requires knowledge of process conditions that the valve will actually see in service. In the industry of control valves it is practice to use flow coefficient and flow characteristics.

In the UK and in the USA coefficient Cv is used and it is defined as flow rate of water in gpm at 60OF that creates pressure drop of 1 psi across the valve. Basic equation for valve sizing for liquid service is:

flow in valve

where is: Cv - flow coefficient [gpm]; q - flow rate [gpm]; Δ p - pressure drop [psi]; S - specific gravity (relative density) [ - ];

To aid in establishing uniform measurement of liquid flow coefficients Cv, standardized testing facility by Fluid Control Institute (FCI) are used by manufacturers. The effect of viscosity of fluids other than water should be considered when selecting the valve, as increased viscosity of fluid is reducing the valve capacity.

Another coefficient Kv is used in some countries, particularly in Europe and is defined as flow rate of water in m3/h that creates pressure drop of 1kg/cm2 across the valve (1 kg/cm2 is equal to 0.980665 bar).

Control valve sizing is based on the calculation of flow coefficient for given pressure drop and flow rate. Liquid flow capacity of a valve in metric units can be converted to Cv as:

flow coeffcient

where is: Cv - flow coefficient [gpm]; qm - flow rate [l/m]; ρ - density [kg/m3]; Δ p - pressure drop [bar];

Also, liquid flow capacity of a valve can be converted to Kv as:

flow coefficient

where is: Kv - flow characteristic [m3/h]; qh - flow rate [m3/h]; S - specific gravity (relative density) [ - ]; Δ p - pressure drop [bar];

Flashing and cavitation, vapor pressure at valve vena contracta

Flashing or cavitation inside a valve can have a significant influence on valve capacity. Flashing and cavitation can reduce the flow through valve in many liquid services. Also, damage can be made to the valve as well as to the piping system. The effect is represented by the change from liquid to vapor state of fluid, resulting in the velocity increase downstream from the valve.

As liquid passes through the restriction area inside the valve flow stream is contracted. The smallest cross section area of stream is just downstream of the actual physical restriction at a point called vena contracta. At that point the velocity is at its maximum and pressure at the minimum.

As the fluid exits the valve, away from vena contracta, velocity decrease and pressure increase, so the critical point for flashing and cavitation is at the point where the pressure is smallest which is in vena contracta. If pressure at vena contracta drops bellows the vapor pressure of the fluid, due to increased velocity at this point, bubbles will form in the flow stream.

If pressure downstream of the vena contracta increase above the vapor pressure, bubbles will collapse or implode producing cavitation. Cavitation releases energy and produces a noise. If cavitation occurs close to solid surfaces, the energy released gradually wears the material leaving the rough surface. Cavitation can also damage the downstream pipeline, if at that place the pressure rises above the vapor pressure and bubbles collapse.

Chocked flow valve pressure drop and cavitation in high pressure recovery valve

Formation of bubbles in the valve resulting of flashing and cavitation effect reduces the flow rate through valve and limits the capacity. This is called chocked flow. Limiting pressure drop in valve is determined by experiment for each valve. Limiting pressure drop for chocked flow in valve can also be calculated using:

chocked flow pressure drop

where is: Δ pallow - maximum allowable pressure drop for chocked flow[psi]; Km - valve recovery coefficient from manufacturer literature [ - ]; p1 - valve inlet absolute pressure [psia]; pv - vapor absolute pressure of the liquid at inlet temperature [psia]; rc - critical pressure ratio 0,70 - 0,95;

In high recovery valve, cavitation can occur on pressure drop below that produces chocked flow. Therefore cavitation index is used to determine the chocked flow pressure drop at which cavitation damage will begin in high recovery valve:

cavitation pressure drop

where is: Kc - cavitation index from manufacturer literature [ - ]; p1 - valve inlet absolute pressure [psia]; pv - vapor absolute pressure of the liquid at inlet temperature [psia]; pc - pressure drop that creates cavitation in high recovery valves [psi];

This equation can be used anytime outlet pressure is greater than the vapor pressure of the liquid.

Flow and discharge through Venturi, nozzle and orifice | Discharge coefficient, pressure and diameter ratio

Orifice plate sizing calculator

Calculate orifice plate diameter, discharge and expansion factor. Applicable for liquids and ideal gases. With orifice plate calculator you can calculate flow rate for measured pressure drop. Calculation is according to ISO 5167.

The rate of flow of any fluid through an orifice or nozzle, may be calculated using following equation:

fluid through an orifice or nozzle

where is: q - flow rate; Cd - coefficient of discharge; A - cross section area; β - diameter ratio d1/d2; gn - acceleration of gravity; hL - head loss;

Instead of coefficient of discharge Cd, more convenient is the use of flow coefficient C which is represented by:

flow coefficient

where is: C - flow coefficient; Cd - coefficient of discharge; β - diameter ratio d1/d2;

Flow rate through nozzles and orifices are than calculated as:

rate through nozzles and orifices

where is: q - flow rate; C - flow coefficient; A - cross section area; Δ p - pressure drop; ρ - density; gn - acceleration of gravity; hL - head loss;

The values of hL and Δ p are measured differential static head or pressure before and after the nozzle or orifice. Values for coefficient of discharge or flow coefficient (C or Cd) can be calculated based on applicable standards like ISO 5167 or similar ASME standards.

Coefficient of discharge for orifice flow can be calculated using Reader-Harris/Gallagher (1998) equation (ISO 5167):

Coefficient of discharge for orifice

where is: β - diameter ratio d1/d2; ReD - Reynolds number based on bigger diameter; d1 - internal diameter (smaller); d2 - internal diameter (larger);

L1 and L2 are functions on tap type and it is:

L1=L2=0 - for corner taps
L1=1; L2=0.47 - for D and D/2 taps
L1=L2=0.0254/d1 - for d1[m] for 1" taps

Coefficient of discharge for Venturi tubes can be obtained based on the type of Venturi tube. There are three types of Venturi tubes and each type has different range of diameters and Reynolds number for which coefficient of discharge is defined as follows:

Venturi tube calculator

Calculate flow rate through Venturi tube based on the created pressure drop by Venturi effect. Calculate velocities on inlet and throat of Venturi tube. Calculate Venturi effect on pressure and velocity in Venturi tube. Applicable for liquids and ideal gases.

Venturi tubes with "as cast" convergent section Cd=0.984; Range for which coefficient of discharge is defined:
100 mm < D < 800 mm
0.3 < β < 0.75
2x10e5 < ReD < 2x10e6

Venturi tubes with a machined convergent section Cd=0.995; Range for which coefficient of discharge is defined:
50 mm < D < 250 mm
0.4 < β < 0.75
2x10e5 < ReD < 2x10e6

Venturi tubes with a rough-welded sheet-iron convergent section Cd=0.985; Range for which coefficient of discharge is defined: 200 mm < D < 1200 mm
0.4 < β < 0.7
2x10e5 < ReD < 2x10e6

Nozzle flow calculator

Calculate flow rate through Nozzle based on the created pressure drop by Venturi effect. Calculate velocities on inlet and throat of Nozzle. For liquids and ideal gases.

Coefficient of discharge for nozzles is calculated based on the type of nozzle in question. For nozzles according to ISA 1932 coefficient of discharge can be calculated using following formula:

Coefficient of dischage for nozzles

Coefficient of discharge for long radius nozzles is calculated using:

Coefficient of disharge for long radius nozzles

and for Venturi type nozzles:

Coefficient of disharge for Venturi nozzles

where is:

β - diameter ratio d1/d2; ReD - Reynolds number based on bigger diameter;

For the flow of compressible fluids through nozzles and orifices, the same equation can be used, but the net expansion factor Y must be included. The flow can be calculated as follows:

compressible flow through nozzles and orifices

where is: Y - expansion factor; C - flow coefficient; A - cross section area; Δ p - pressure drop; ρ - density;

The expansion factor Y depends on the specific heat ratio χ , the diameter ratio β and the ratio of downstream and upstream absolute pressures.

Expansion factor Y for Venturi tubes and nozzles can be calculated as follows (ISO 5167):

expansion factor

This equation is applicable for the same range of diameter and Reynolds number as for coefficient of discharge Cd indicated above. Formula is applicable only for pressure ratio p2/p1 > 0.75.

For compressible flow through orifices expansion factor is (ISO 5167):

expansion factor

where is: Y - expansion factor; χ - specific heat ratio; β - diameter ratio d1/d2; p1 - inlet pressure; p2 - pressure in Venturi throat or after the orifice or nozzle;

This equation can be used for gas flow though the orifice and discharging to the atmosphere. For that purpose the pressure difference equals to the upstream gauge pressure. This applies only if absolute atmospheric pressure divided by absolute upstream pressure is bigger than critical pressure ratio for sonic flow conditions.

When the smoothly convergent nozzle is used compressible fluid can reach the speed of sound at minimum cross section or throat, if upstream pressure is high enough.

When the velocity of compressible fluid reaches the speed of sound, maximum flow has been reached, and increase of upstream pressure or decrease of downstream pressure will not increase the flow any more.

For short tubes where relation L/D is not bigger than 2.5 the flow of discharge to the atmosphere can be calculated using above equations, with flow coefficient C somewhere between the values for orifice and nozzle.

If the entrance to the short tube is well rounded then the flow coefficient C for nozzles can be used and if the pipe entrance is square shaped and sharp then flow coefficient C for orifice is more appropriate.

Flow discharge through valves, fittings and pipe, resistance coefficient K

For discharge of liquids through valves, fittings and pipes Darcy formula can be expressed as:

liquid discharge

where is:

q - discharge flow rate [l/min]; d - internal pipe diameter [mm]; hL - head loss [m]; K - resistance coefficient [ - ];

This equation can be used for offtake calculation from pipes, fittings and valves when resistance coefficient K, static head difference hL and internal pipe diameter d is known. The resistance coefficient is the sum of all resistances in the piping system.

Gas offtake calculator

Calculate gas flow rate when discharging from pipe or reservoir. Calculation of gas offtake through pipe, valve or orifice in reservoir. Chocked flow condition check included.

For offtake of compressible flow of fluid from a pipe to a larger area or larger cross section like in the case of offtake to the atmosphere, a modified Darcy formula can be used:

gas offtake

where is:

w - offtake mass flow rate [kg/s]; Y - expansion factor [ - ]; d - internal pipe diameter [mm]; Δ p - pressure drop [Pa]; ρ - density [kg/m3]; K - resistance coefficient [ - ];

Gas pressure regulator capacity - flow coefficient Cg, Kg | Critical flow rate

For gas pressure regulators that are operating in the range of inlet pressure up to 100 bar following equations for sub-critical and critical flow behavior are used (EN 334):

Sub-critical flow:

gas valve capacity

Critical flow:

gas valve capacity

Gas control valve sizing calculator

Calculate flow coefficient Cg or Kg or maximum capacity of control valve for known upstream and downstream pressure. Calculate pressure drop that control valve is creating for known flow rate and flow coefficient Cg or Kg.

where is:

Q - gas flow rate [m3/h]; S - gas relative density (for air=1) [ - ]; tu - gas upstream temperature [OC]; Cg - gas flow coefficient [ - ]; pu - gas upstream pressure [bar]; pd - gas downstream pressure [bar]; pb - ambient atmospheric pressure [bar]; K1 - valve body shape factor [ - ];

Simplified calculation can be used if K1 < 130 and (pu-pd) > 0,1 (pu+pb):

Sub-critical flow rate where (pu-pd) < 0,5 (pu+pb):

gas valve capacity

Sub-critical flow rate where (pu-pd) > 0,5 (pu+pb):

gas valve capacity

Above equation can be expressed with flow coefficient Kg included as:

gas valve capacity

With above equations when flow coefficient Cg or Kg from gas pressure regulator manufacturer is known, regulator capacity can be calculated for given pressures upstream and downstream from gas regulator.

It can be concluded that if pressure of gas before and after the regulator are higher, capacity of regulator will also be higher for the same type and dimension of regulator.

When flow rate through regulator is critical, pressure downstream of the regulator doesn't influence the regulator capacity.

It is important also to notice that for different type of gases that have different value of density, capacity of regulator will also change, and for gases with higher densities, flow rate will be smaller and volume capacity will drop.

All equations are for regulators with fully opened control element, as flow coefficient are measured for fully opened regulator. Capacities for different positions of control element in regulator are calculated related to the curve of appropriate regulator.

Natural gas control valve flow rate for pressure ratio at normal conditions

For control valves in natural gas industry it is common to use KG which is defined for under critical pressure ratio (pa/pe > 0.54) as:

KG flow coefficient

For overcritical pressure ratio (pa/pe < 0.54):

KG flow coefficient

where is:

KG - flow coefficient [m3/h] qn - flow rate at normal conditions (p = 101325 Pa, T = 273,15 K) [m3/h] pa - pressure after the control valve [bar] pe - pressure in front of the control valve [bar]

For other gases, correction factor should be used as:

flow of other gases

where is correction factor:

correction factor

where is:

qn NATURAL GAS - flow rate at normal conditions of natural gas [m3/h] qn GAS - flow rate at normal conditions of other gas [m3/h] f - correction factor [ - ]

  • Pipe flow theory pages
  • Fluid properties
    Fluid density, specific volume, specific gravity, mixture density, viscosity, pressure levels
  • Incompressible flow in pipe
    Pipe diameter, Reynolds number, laminar/turbulent flow, Darcy formula, friction factor, dynamic/total pressure, heat energy
  • Flow in valves and fittings
    Resistance coefficient, flow coefficient, cavitation, chocked flow, flow offtake, gas regulator, natural gas control valves
  • Compressible flow
    Adiabatic, isothermal flow, fuel combustion, maximum flow, evaporation energy
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