Velocity at any point for coefficient of pitot-tube Solution

STEP 0: Pre-Calculation Summary
Formula Used
Velocity at Any Point for Pitot Tube = Coefficient of Pitot Tube*sqrt(2*9.81*Rise of Liquid in Pitot Tube)
Vpitot = Cv*sqrt(2*9.81*hp)
This formula uses 1 Functions, 3 Variables
Functions Used
sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)
Variables Used
Velocity at Any Point for Pitot Tube - (Measured in Meter per Second) - Velocity at any point for pitot tube is the velocity of fluid at any point calculated using the pitot tube.
Coefficient of Pitot Tube - The Coefficient of Pitot Tube is the ratio of actual velocity to the theoretical velocity of the fluid in the pitot tube.
Rise of Liquid in Pitot Tube - (Measured in Meter) - Rise of liquid in pitot tube is the rise of liquid in the pitot tube above the free surface.
STEP 1: Convert Input(s) to Base Unit
Coefficient of Pitot Tube: 0.98 --> No Conversion Required
Rise of Liquid in Pitot Tube: 210.5 Centimeter --> 2.105 Meter (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Vpitot = Cv*sqrt(2*9.81*hp) --> 0.98*sqrt(2*9.81*2.105)
Evaluating ... ...
Vpitot = 6.2979850777848
STEP 3: Convert Result to Output's Unit
6.2979850777848 Meter per Second --> No Conversion Required
FINAL ANSWER
6.2979850777848 6.297985 Meter per Second <-- Velocity at Any Point for Pitot Tube
(Calculation completed in 00.004 seconds)

Credits

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PSG College of Technology (PSGCT), Coimbatore
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17 Kinematics of Flow Calculators

Actual Discharge in Venturimeter
Go Actual Discharge through Venturimeter = Coefficient of Discharge of Venturimeter*((Cross Section Area of Venturimeter Inlet*Cross Section Area of Venturimeter Throat)/(sqrt((Cross Section Area of Venturimeter Inlet^2)-(Cross Section Area of Venturimeter Throat^2)))*sqrt(2*[g]*Net Head of Liquid in Venturimeter))
Relative velocity of fluid with respect to body given drag force
Go Relative Velocity of Fluid Past Body = sqrt((Drag Force by Fluid on Body*2)/(Projected Area of Body*Density of Moving Fluid*Drag Coefficient for Fluid Flow))
Drag coefficient given Drag force
Go Drag Coefficient for Fluid Flow = (Drag Force by Fluid on Body*2)/(Projected Area of Body*Density of Moving Fluid*Relative Velocity of Fluid Past Body^2)
Difference in pressure head for light liquid in manometer
Go Difference in Pressure Head in Manometer = Difference in Liquid Level in Manometer*(1-(Specific Gravity of Lighter Liquid/Specific Gravity of Flowing Liquid))
Difference in Pressure Head for heavier Liquid in Manometer
Go Difference in Pressure Head in Manometer = Difference in Liquid Level in Manometer*(Specific Gravity of Heavier Liquid/Specific Gravity of Flowing Liquid-1)
Total Pressure Force at Bottom of Cylinder
Go Pressure Force on Bottom = Density*9.81*pi*(Radius^2)*Cylinder Height+Pressure Force on Top
Resultant bend force along x and y direction
Go Resultant Force on Pipe Bend = sqrt((Force along X-Direction on Pipe Bend^2)+(Force along Y-Direction on Pipe Bend^2))
Height or depth of paraboloid for volume of air
Go Height of Crack = ((Diameter^2)/(2*(Radius^2)))*(Length-Initial Height of Liquid)
Total pressure force on top of cylinder
Go Pressure Force on Top = (Liquid Density/4)*(Angular Velocity^2)*pi*(Radius^4)
Coefficient of pitot-tube for velocity at any point
Go Coefficient of Pitot Tube = Velocity at Any Point for Pitot Tube/(sqrt(2*9.81*Rise of Liquid in Pitot Tube))
Velocity at any point for coefficient of pitot-tube
Go Velocity at Any Point for Pitot Tube = Coefficient of Pitot Tube*sqrt(2*9.81*Rise of Liquid in Pitot Tube)
Resultant velocity for two velocity components
Go Resultant Velocity = sqrt((Velocity Component at U^2)+(Velocity Component at V^2))
Angular Velocity of Vortex using Depth of Parabola
Go Angular Velocity = sqrt((Depth of Parabola*2*9.81)/(Radius^2))
Depth of Parabola formed at Free Surface of Water
Go Depth of Parabola = ((Angular Velocity^2)*(Radius^2))/(2*9.81)
Velocity of Fluid Particle
Go Velocity of Fluid Particle = Displacement/Total Time Taken
Rate of flow or discharge
Go Rate of Flow = Cross-Sectional Area*Average Velocity
Air Resistance Force
Go Air Resistance = Air Constant*Velocity^2

Velocity at any point for coefficient of pitot-tube Formula

Velocity at Any Point for Pitot Tube = Coefficient of Pitot Tube*sqrt(2*9.81*Rise of Liquid in Pitot Tube)
Vpitot = Cv*sqrt(2*9.81*hp)

What is the principle of pitot-tube?

The pitot tube is a differential pressure measuring device. The pitot tube installed in the flow stream measures the direct pressure at the contact pitot tube hole and a second measurement is required, being of static pressure.

How does a pitot-tube measure velocity?

A Pitot tube measures total pressure and static pressure to determine the velocity pressure from which air velocity can be derived. The Pitot tube is inserted into the duct with the tip pointed toward the airflow.

How to Calculate Velocity at any point for coefficient of pitot-tube?

Velocity at any point for coefficient of pitot-tube calculator uses Velocity at Any Point for Pitot Tube = Coefficient of Pitot Tube*sqrt(2*9.81*Rise of Liquid in Pitot Tube) to calculate the Velocity at Any Point for Pitot Tube, The Velocity at any point for coefficient of pitot-tube formula is known while considering the rise of the liquid in the tube above the free surface which is the height of the liquid in the top edge of pitot-tube. Velocity at Any Point for Pitot Tube is denoted by Vpitot symbol.

How to calculate Velocity at any point for coefficient of pitot-tube using this online calculator? To use this online calculator for Velocity at any point for coefficient of pitot-tube, enter Coefficient of Pitot Tube (Cv) & Rise of Liquid in Pitot Tube (hp) and hit the calculate button. Here is how the Velocity at any point for coefficient of pitot-tube calculation can be explained with given input values -> 6.297985 = 0.98*sqrt(2*9.81*2.105).

FAQ

What is Velocity at any point for coefficient of pitot-tube?
The Velocity at any point for coefficient of pitot-tube formula is known while considering the rise of the liquid in the tube above the free surface which is the height of the liquid in the top edge of pitot-tube and is represented as Vpitot = Cv*sqrt(2*9.81*hp) or Velocity at Any Point for Pitot Tube = Coefficient of Pitot Tube*sqrt(2*9.81*Rise of Liquid in Pitot Tube). The Coefficient of Pitot Tube is the ratio of actual velocity to the theoretical velocity of the fluid in the pitot tube & Rise of liquid in pitot tube is the rise of liquid in the pitot tube above the free surface.
How to calculate Velocity at any point for coefficient of pitot-tube?
The Velocity at any point for coefficient of pitot-tube formula is known while considering the rise of the liquid in the tube above the free surface which is the height of the liquid in the top edge of pitot-tube is calculated using Velocity at Any Point for Pitot Tube = Coefficient of Pitot Tube*sqrt(2*9.81*Rise of Liquid in Pitot Tube). To calculate Velocity at any point for coefficient of pitot-tube, you need Coefficient of Pitot Tube (Cv) & Rise of Liquid in Pitot Tube (hp). With our tool, you need to enter the respective value for Coefficient of Pitot Tube & Rise of Liquid in Pitot Tube and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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