Flow Velocity given Thrust on Propeller Solution

STEP 0: Pre-Calculation Summary
Formula Used
Flow Velocity = -(Thrust Force/(Water Density*Rate of Flow))+Absolute Velocity of Issuing Jet
Vf = -(Ft/(ρWater*qflow))+V
This formula uses 5 Variables
Variables Used
Flow Velocity - (Measured in Meter per Second) - Flow Velocity is the velocity of the flow of any fluid.
Thrust Force - (Measured in Newton) - Thrust Force acting perpendicular to the job piece.
Water Density - (Measured in Kilogram per Cubic Meter) - Water Density is mass per unit of water.
Rate of Flow - (Measured in Cubic Meter per Second) - Rate of Flow is the rate at which a liquid or other substance flows through a particular channel, pipe, etc.
Absolute Velocity of Issuing Jet - (Measured in Meter per Second) - Absolute Velocity of Issuing Jet is actual velocity of jet used in propeller.
STEP 1: Convert Input(s) to Base Unit
Thrust Force: 0.5 Kilonewton --> 500 Newton (Check conversion ​here)
Water Density: 1000 Kilogram per Cubic Meter --> 1000 Kilogram per Cubic Meter No Conversion Required
Rate of Flow: 24 Cubic Meter per Second --> 24 Cubic Meter per Second No Conversion Required
Absolute Velocity of Issuing Jet: 6 Meter per Second --> 6 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Vf = -(Ft/(ρWater*qflow))+V --> -(500/(1000*24))+6
Evaluating ... ...
Vf = 5.97916666666667
STEP 3: Convert Result to Output's Unit
5.97916666666667 Meter per Second --> No Conversion Required
FINAL ANSWER
5.97916666666667 5.979167 Meter per Second <-- Flow Velocity
(Calculation completed in 00.004 seconds)

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National Institute of Technology Karnataka (NITK), Surathkal
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14 Momentum Theory of Propellers Calculators

Output Power given Rate of Flow through Propeller
​ Go Output Power = Water Density*Rate of Flow*Flow Velocity*(Absolute Velocity of Issuing Jet-Flow Velocity)
Flow Velocity given Power Lost
​ Go Flow Velocity = Absolute Velocity of Issuing Jet-sqrt((Power Loss/(Density of Fluid*Rate of Flow*0.5)))
Rate of Flow through Propeller
​ Go Rate of Flow through Propeller = (pi/8)*(Diameter of Turbine^2)*(Absolute Velocity of Issuing Jet+Flow Velocity)
Rate of Flow given Power Lost
​ Go Rate of Flow = Power Loss/Density of Fluid*0.5*(Absolute Velocity of Issuing Jet-Flow Velocity)^2
Power Lost
​ Go Power Loss = Density of Fluid*Rate of Flow*0.5*(Absolute Velocity of Issuing Jet-Flow Velocity)^2
Flow Velocity given Rate of Flow through Propeller
​ Go Flow Velocity = (8*Rate of Flow/(pi*Diameter of Turbine^2))-Absolute Velocity of Issuing Jet
Flow Velocity given Thrust on Propeller
​ Go Flow Velocity = -(Thrust Force/(Water Density*Rate of Flow))+Absolute Velocity of Issuing Jet
Diameter of Propeller given Thrust on Propeller
​ Go Diameter of Turbine = sqrt((4/pi)*Thrust Force/Change in Pressure)
Thrust on Propeller
​ Go Thrust Force = (pi/4)*(Diameter of Turbine^2)*Change in Pressure
Theoretical Propulsive Efficiency
​ Go Efficiency of Jet = 2/(1+(Absolute Velocity of Issuing Jet/Flow Velocity))
Flow Velocity given Theoretical Propulsive efficiency
​ Go Flow Velocity = Absolute Velocity of Issuing Jet/(2/Efficiency of Jet-1)
Output Power given Input Power
​ Go Output Power = Total Input Power-Power Loss
Power Lost given Input Power
​ Go Power Loss = Total Input Power-Output Power
Input Power
​ Go Total Input Power = Output Power+Power Loss

Flow Velocity given Thrust on Propeller Formula

Flow Velocity = -(Thrust Force/(Water Density*Rate of Flow))+Absolute Velocity of Issuing Jet
Vf = -(Ft/(ρWater*qflow))+V

What is Rate of Flow?

Rate of flow may refer to: Mass flow rate, the movement of mass per time. Volumetric flow rate, the volume of a fluid which passes through a given surface per unit of time. Heat flow rate, the movement of heat per time.

How to Calculate Flow Velocity given Thrust on Propeller?

Flow Velocity given Thrust on Propeller calculator uses Flow Velocity = -(Thrust Force/(Water Density*Rate of Flow))+Absolute Velocity of Issuing Jet to calculate the Flow Velocity, The Flow Velocity given Thrust on Propeller is defined as velocity of discharge of fluid on jet. Flow Velocity is denoted by Vf symbol.

How to calculate Flow Velocity given Thrust on Propeller using this online calculator? To use this online calculator for Flow Velocity given Thrust on Propeller, enter Thrust Force (Ft), Water Density Water), Rate of Flow (qflow) & Absolute Velocity of Issuing Jet (V) and hit the calculate button. Here is how the Flow Velocity given Thrust on Propeller calculation can be explained with given input values -> 7.979167 = -(500/(1000*24))+6.

FAQ

What is Flow Velocity given Thrust on Propeller?
The Flow Velocity given Thrust on Propeller is defined as velocity of discharge of fluid on jet and is represented as Vf = -(Ft/(ρWater*qflow))+V or Flow Velocity = -(Thrust Force/(Water Density*Rate of Flow))+Absolute Velocity of Issuing Jet. Thrust Force acting perpendicular to the job piece, Water Density is mass per unit of water, Rate of Flow is the rate at which a liquid or other substance flows through a particular channel, pipe, etc & Absolute Velocity of Issuing Jet is actual velocity of jet used in propeller.
How to calculate Flow Velocity given Thrust on Propeller?
The Flow Velocity given Thrust on Propeller is defined as velocity of discharge of fluid on jet is calculated using Flow Velocity = -(Thrust Force/(Water Density*Rate of Flow))+Absolute Velocity of Issuing Jet. To calculate Flow Velocity given Thrust on Propeller, you need Thrust Force (Ft), Water Density Water), Rate of Flow (qflow) & Absolute Velocity of Issuing Jet (V). With our tool, you need to enter the respective value for Thrust Force, Water Density, Rate of Flow & Absolute Velocity of Issuing Jet 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 Flow Velocity?
In this formula, Flow Velocity uses Thrust Force, Water Density, Rate of Flow & Absolute Velocity of Issuing Jet. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Flow Velocity = (8*Rate of Flow/(pi*Diameter of Turbine^2))-Absolute Velocity of Issuing Jet
  • Flow Velocity = Absolute Velocity of Issuing Jet-sqrt((Power Loss/(Density of Fluid*Rate of Flow*0.5)))
  • Flow Velocity = Absolute Velocity of Issuing Jet/(2/Efficiency of Jet-1)
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