Area of Hole given Coefficient of Velocity for Jet Solution

STEP 0: Pre-Calculation Summary
Formula Used
Cross Sectional Area of Jet = (0.5*Force of Fluid)/(Specific Weight of Liquid*Impulse Height*Coefficient of Velocity^2)
AJet = (0.5*F)/(γf*h*Cv^2)
This formula uses 5 Variables
Variables Used
Cross Sectional Area of Jet - (Measured in Square Meter) - Cross Sectional Area of Jet is the area of a two-dimensional shape that is obtained when a three-dimensional shape is sliced perpendicular to some specified axis at a point.
Force of Fluid - (Measured in Newton) - Force of Fluid is the force resulting from liquid pressure acting over an area.
Specific Weight of Liquid - (Measured in Kilonewton per Cubic Meter) - Specific Weight of Liquid represents the force exerted by gravity on a unit volume of a fluid.
Impulse Height - (Measured in Meter) - Impulse height is the distance between the lowest and highest points of a person/ shape/ object standing upright.
Coefficient of Velocity - The Coefficient of Velocity is the ratio of actual velocity to theoretical velocity.
STEP 1: Convert Input(s) to Base Unit
Force of Fluid: 240 Newton --> 240 Newton No Conversion Required
Specific Weight of Liquid: 9.81 Kilonewton per Cubic Meter --> 9.81 Kilonewton per Cubic Meter No Conversion Required
Impulse Height: 12.11 Meter --> 12.11 Meter No Conversion Required
Coefficient of Velocity: 0.92 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
AJet = (0.5*F)/(γf*h*Cv^2) --> (0.5*240)/(9.81*12.11*0.92^2)
Evaluating ... ...
AJet = 1.1934176068518
STEP 3: Convert Result to Output's Unit
1.1934176068518 Square Meter --> No Conversion Required
FINAL ANSWER
1.1934176068518 1.193418 Square Meter <-- Cross Sectional Area of Jet
(Calculation completed in 00.004 seconds)

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National Institute of Technology Karnataka (NITK), Surathkal
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7 Jet Propulsion of Orifice Tank Calculators

Actual Velocity given Force exerted on Tank due to Jet
Go Actual Velocity = sqrt((Force of Fluid*[g])/(Specific Weight of Liquid*Cross Sectional Area of Jet))
Head over Jet Hole given Force exerted on Tank due to Jet
Go Impulse Height = (0.5*Force of Fluid)/((Coefficient of Velocity^2)*Specific Weight of Liquid*Cross Sectional Area of Jet)
Specific Weight of Liquid given Coefficient of Velocity for Jet
Go Specific Weight of Liquid = (0.5*Force of Fluid)/(Cross Sectional Area of Jet*Impulse Height*Coefficient of Velocity^2)
Area of Hole given Coefficient of Velocity for Jet
Go Cross Sectional Area of Jet = (0.5*Force of Fluid)/(Specific Weight of Liquid*Impulse Height*Coefficient of Velocity^2)
Specific Weight of Liquid given Force exerted on Tank due to Jet
Go Specific Weight of Liquid = ((Force of Fluid*[g])/(Cross Sectional Area of Jet*(Actual Velocity)^2))
Area of Jet given Force exerted on Tank due to Jet
Go Cross Sectional Area of Jet = Force of Fluid/(Specific Weight of Liquid*(Actual Velocity^2)/[g])
Force exerted on Tank due to Jet
Go Force of Fluid = Specific Weight of Liquid*Cross Sectional Area of Jet*(Actual Velocity^2)/[g]

Area of Hole given Coefficient of Velocity for Jet Formula

Cross Sectional Area of Jet = (0.5*Force of Fluid)/(Specific Weight of Liquid*Impulse Height*Coefficient of Velocity^2)
AJet = (0.5*F)/(γf*h*Cv^2)

How do you measure the velocity of a jet?

Velocity measurements are carried out with a spring dynamometer and a free-running Pelton micro turbine. The jet strength at the outlet of the nozzle is found to increase by a factor of 4.0–4.5 compared with the water flow strength at the inlet, which depends on the excess pressure and volume flow at the inlet.

How to Calculate Area of Hole given Coefficient of Velocity for Jet?

Area of Hole given Coefficient of Velocity for Jet calculator uses Cross Sectional Area of Jet = (0.5*Force of Fluid)/(Specific Weight of Liquid*Impulse Height*Coefficient of Velocity^2) to calculate the Cross Sectional Area of Jet, The Area of Hole given Coefficient of Velocity for Jet is defined as area made on the tank surface for ejection. Cross Sectional Area of Jet is denoted by AJet symbol.

How to calculate Area of Hole given Coefficient of Velocity for Jet using this online calculator? To use this online calculator for Area of Hole given Coefficient of Velocity for Jet, enter Force of Fluid (F), Specific Weight of Liquid f), Impulse Height (h) & Coefficient of Velocity (Cv) and hit the calculate button. Here is how the Area of Hole given Coefficient of Velocity for Jet calculation can be explained with given input values -> 1.193418 = (0.5*240)/(9810*12.11*0.92^2).

FAQ

What is Area of Hole given Coefficient of Velocity for Jet?
The Area of Hole given Coefficient of Velocity for Jet is defined as area made on the tank surface for ejection and is represented as AJet = (0.5*F)/(γf*h*Cv^2) or Cross Sectional Area of Jet = (0.5*Force of Fluid)/(Specific Weight of Liquid*Impulse Height*Coefficient of Velocity^2). Force of Fluid is the force resulting from liquid pressure acting over an area, Specific Weight of Liquid represents the force exerted by gravity on a unit volume of a fluid, Impulse height is the distance between the lowest and highest points of a person/ shape/ object standing upright & The Coefficient of Velocity is the ratio of actual velocity to theoretical velocity.
How to calculate Area of Hole given Coefficient of Velocity for Jet?
The Area of Hole given Coefficient of Velocity for Jet is defined as area made on the tank surface for ejection is calculated using Cross Sectional Area of Jet = (0.5*Force of Fluid)/(Specific Weight of Liquid*Impulse Height*Coefficient of Velocity^2). To calculate Area of Hole given Coefficient of Velocity for Jet, you need Force of Fluid (F), Specific Weight of Liquid f), Impulse Height (h) & Coefficient of Velocity (Cv). With our tool, you need to enter the respective value for Force of Fluid, Specific Weight of Liquid, Impulse Height & Coefficient of Velocity and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Cross Sectional Area of Jet?
In this formula, Cross Sectional Area of Jet uses Force of Fluid, Specific Weight of Liquid, Impulse Height & Coefficient of Velocity. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Cross Sectional Area of Jet = Force of Fluid/(Specific Weight of Liquid*(Actual Velocity^2)/[g])
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