Kinetic Energy of Air at Inlet Calculator

✖Mass flow rate of air is the mass flow rate of air.ⓘ Mass Flow Rate of Air [m_a]			+10% -10%
✖Aircraft forward speed the speed at which aircraft is moving.ⓘ Aircraft Forward Speed [V]			+10% -10%

✖Kinetic Energy is defined as the energy possessed by a moving fluid.ⓘ Kinetic Energy of Air at Inlet [KE]

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Kinetic Energy of Air at Inlet Solution

STEP 0: Pre-Calculation Summary

Formula Used

Kinetic Energy = 1/2*Mass Flow Rate of Air*Aircraft Forward Speed^2
KE = 1/2*m_a*V^2
This formula uses 3 Variables

Variables Used

Kinetic Energy - (Measured in Joule) - Kinetic Energy is defined as the energy possessed by a moving fluid.
Mass Flow Rate of Air - (Measured in Kilogram per Second) - Mass flow rate of air is the mass flow rate of air.
Aircraft Forward Speed - (Measured in Meter per Second) - Aircraft forward speed the speed at which aircraft is moving.

STEP 1: Convert Input(s) to Base Unit

Mass Flow Rate of Air: 3.5 Kilogram per Second --> 3.5 Kilogram per Second No Conversion Required
Aircraft Forward Speed: 124 Meter per Second --> 124 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

KE = 1/2*m_a*V^2 --> 1/2*3.5*124^2

Evaluating ... ...

KE = 26908

STEP 3: Convert Result to Output's Unit

26908 Joule -->26.908 Kilojoule (Check conversion here)

FINAL ANSWER

26.908 Kilojoule <-- Kinetic Energy

(Calculation completed in 00.004 seconds)

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Home » Physics » Propulsion » Components of Gas Turbine » Aerospace » Inlets » Kinetic Energy of Air at Inlet

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 Sagar S Kulkarni

Dayananda Sagar College of Engineering (DSCE), Bengaluru

Sagar S Kulkarni has verified this Calculator and 200+ more calculators!

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Kinetic Energy of Air at Inlet

LaTeX Go Kinetic Energy = 1/2*Mass Flow Rate of Air*Aircraft Forward Speed^2

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Kinetic Energy of Air at Inlet Formula

LaTeX Go

Kinetic Energy = 1/2*Mass Flow Rate of Air*Aircraft Forward Speed^2
KE = 1/2*m_a*V^2

What is kinetic energy?

kinetic energy of an object is the energy that it possesses due to its motion. It is defined as the work needed to accelerate a body of a given mass from rest to its stated velocity.

How to Calculate Kinetic Energy of Air at Inlet?

Kinetic Energy of Air at Inlet calculator uses Kinetic Energy = 1/2*Mass Flow Rate of Air*Aircraft Forward Speed^2 to calculate the Kinetic Energy, The Kinetic energy of air at inlet formula is defined as the half of the product of mass flow rate of air and square of aircraft forward speed. Kinetic Energy is denoted by KE symbol.

How to calculate Kinetic Energy of Air at Inlet using this online calculator? To use this online calculator for Kinetic Energy of Air at Inlet, enter Mass Flow Rate of Air (m_a) & Aircraft Forward Speed (V) and hit the calculate button. Here is how the Kinetic Energy of Air at Inlet calculation can be explained with given input values -> 26908 = 1/2*3.5*124^2.

FAQ

What is Kinetic Energy of Air at Inlet?

The Kinetic energy of air at inlet formula is defined as the half of the product of mass flow rate of air and square of aircraft forward speed and is represented as KE = 1/2*m_a*V^2 or Kinetic Energy = 1/2*Mass Flow Rate of Air*Aircraft Forward Speed^2. Mass flow rate of air is the mass flow rate of air & Aircraft forward speed the speed at which aircraft is moving.

How to calculate Kinetic Energy of Air at Inlet?

The Kinetic energy of air at inlet formula is defined as the half of the product of mass flow rate of air and square of aircraft forward speed is calculated using Kinetic Energy = 1/2*Mass Flow Rate of Air*Aircraft Forward Speed^2. To calculate Kinetic Energy of Air at Inlet, you need Mass Flow Rate of Air (m_a) & Aircraft Forward Speed (V). With our tool, you need to enter the respective value for Mass Flow Rate of Air & Aircraft Forward Speed 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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