Energy Transfer due to Change of Relative Kinetic Energy of Fluid Calculator

✖Relative Velocity at Exit will be observed by an observer positioned on the rotor.ⓘ Relative Velocity at Exit [w₂]			+10% -10%
✖Relative Velocity at Inlet which will be observed by an observer positioned on the rotor.ⓘ Relative Velocity at Inlet [w₁]			+10% -10%

✖Energy Transfer refers to the process by which energy is transmitted or moved from one object or system to another.ⓘ Energy Transfer due to Change of Relative Kinetic Energy of Fluid [E]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Jet Propulsion Formula PDF PDF Image

Energy Transfer due to Change of Relative Kinetic Energy of Fluid Solution

STEP 0: Pre-Calculation Summary

Formula Used

Energy Transfer = (Relative Velocity at Exit^2-Relative Velocity at Inlet^2)/2
E = (w₂^2-w₁^2)/2
This formula uses 3 Variables

Variables Used

Energy Transfer - (Measured in Joule) - Energy Transfer refers to the process by which energy is transmitted or moved from one object or system to another.
Relative Velocity at Exit - (Measured in Meter per Second) - Relative Velocity at Exit will be observed by an observer positioned on the rotor.
Relative Velocity at Inlet - (Measured in Meter per Second) - Relative Velocity at Inlet which will be observed by an observer positioned on the rotor.

STEP 1: Convert Input(s) to Base Unit

Relative Velocity at Exit: 96 Meter per Second --> 96 Meter per Second No Conversion Required
Relative Velocity at Inlet: 48 Meter per Second --> 48 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

E = (w₂^2-w₁^2)/2 --> (96^2-48^2)/2

Evaluating ... ...

E = 3456

STEP 3: Convert Result to Output's Unit

3456 Joule -->3.456 Kilojoule (Check conversion here)

FINAL ANSWER

3.456 Kilojoule <-- Energy Transfer

(Calculation completed in 00.004 seconds)

You are here -

Home » Physics » Propulsion » Jet Propulsion » Aerospace » Turbomachinery Equations » Energy Transfer due to Change of Relative Kinetic Energy of Fluid

Credits

Created by Chilvera Bhanu Teja

Institute of Aeronautical Engineering (IARE), Hyderabad

Chilvera Bhanu Teja has created this Calculator and 300+ more calculators!

Verified by Anshika Arya

National Institute Of Technology (NIT), Hamirpur

Anshika Arya has verified this Calculator and 2500+ more calculators!

< Turbomachinery Equations Calculators

Peripheral Velocity of Blade at Entry corresponding to Diameter

LaTeX Go Peripheral Velocity at Inlet = (pi*Blade Diameter at Inlet*Speed in RPM)/60

Peripheral Velocity of Blade at Exit corresponding to Diameter

LaTeX Go Peripheral Velocity at Exit = (pi*Blade Diameter at Exit*Speed in RPM)/60

Angular Moment of Momentum at Inlet

LaTeX Go Angular Momentum = Tangential Velocity at Inlet*Inlet Radius

Angular Moment of Momentum at Exit

LaTeX Go Angular Momentum = Tangential Velocity at Exit*Exit Radius

Energy Transfer due to Change of Relative Kinetic Energy of Fluid Formula

LaTeX Go

Energy Transfer = (Relative Velocity at Exit^2-Relative Velocity at Inlet^2)/2
E = (w₂^2-w₁^2)/2

What is energy?

Energy is the quantitative property that must be transferred to an object in order to perform work on, or to heat, the object. Energy is a conserved quantity; the law of conservation of energy states that energy can be converted in form, but not created or destroyed.

How to Calculate Energy Transfer due to Change of Relative Kinetic Energy of Fluid?

Energy Transfer due to Change of Relative Kinetic Energy of Fluid calculator uses Energy Transfer = (Relative Velocity at Exit^2-Relative Velocity at Inlet^2)/2 to calculate the Energy Transfer, The Energy transfer due to change of relative kinetic energy of fluid formula is defined as the half of the difference of the square of relative velocities at exit and inlet. Energy Transfer is denoted by E symbol.

How to calculate Energy Transfer due to Change of Relative Kinetic Energy of Fluid using this online calculator? To use this online calculator for Energy Transfer due to Change of Relative Kinetic Energy of Fluid, enter Relative Velocity at Exit (w₂) & Relative Velocity at Inlet (w₁) and hit the calculate button. Here is how the Energy Transfer due to Change of Relative Kinetic Energy of Fluid calculation can be explained with given input values -> 0.003456 = (96^2-48^2)/2.

FAQ

What is Energy Transfer due to Change of Relative Kinetic Energy of Fluid?

The Energy transfer due to change of relative kinetic energy of fluid formula is defined as the half of the difference of the square of relative velocities at exit and inlet and is represented as E = (w₂^2-w₁^2)/2 or Energy Transfer = (Relative Velocity at Exit^2-Relative Velocity at Inlet^2)/2. Relative Velocity at Exit will be observed by an observer positioned on the rotor & Relative Velocity at Inlet which will be observed by an observer positioned on the rotor.

How to calculate Energy Transfer due to Change of Relative Kinetic Energy of Fluid?

The Energy transfer due to change of relative kinetic energy of fluid formula is defined as the half of the difference of the square of relative velocities at exit and inlet is calculated using Energy Transfer = (Relative Velocity at Exit^2-Relative Velocity at Inlet^2)/2. To calculate Energy Transfer due to Change of Relative Kinetic Energy of Fluid, you need Relative Velocity at Exit (w₂) & Relative Velocity at Inlet (w₁). With our tool, you need to enter the respective value for Relative Velocity at Exit & Relative Velocity at Inlet 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 Energy Transfer?

In this formula, Energy Transfer uses Relative Velocity at Exit & Relative Velocity at Inlet. We can use 2 other way(s) to calculate the same, which is/are as follows -

Energy Transfer = (Absolute Velocity at Inlet^2-Absolute Velocity at Exit^2)/2
Energy Transfer = (Peripheral Velocity at Inlet^2-Peripheral Velocity at Exit^2)/2

Home

FREE PDFs

🔍 Search