Velocity after Expansion given Ideal Thrust Calculator

✖Ideal Thrust is the thrust produced by an engine when nozzle exit pressure is same as ambient pressure or nozzle is perfectly expanded.ⓘ Ideal Thrust [T_ideal]			+10% -10%
✖Mass Flow Rate represents the amount of mass passing through a system per unit of time.ⓘ Mass Flow Rate [m_a]			+10% -10%
✖Flight Speed refers to the velocity at which an aircraft moves through the air.ⓘ Flight Speed [V]			+10% -10%

✖Exit Velocity refers to the speed at which gases expand at the exit of nozzle of a engine.ⓘ Velocity after Expansion given Ideal Thrust [V_e]

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Velocity after Expansion given Ideal Thrust Solution

STEP 0: Pre-Calculation Summary

Formula Used

Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed
V_e = T_ideal/m_a+V
This formula uses 4 Variables

Variables Used

Exit Velocity - (Measured in Meter per Second) - Exit Velocity refers to the speed at which gases expand at the exit of nozzle of a engine.
Ideal Thrust - (Measured in Newton) - Ideal Thrust is the thrust produced by an engine when nozzle exit pressure is same as ambient pressure or nozzle is perfectly expanded.
Mass Flow Rate - (Measured in Kilogram per Second) - Mass Flow Rate represents the amount of mass passing through a system per unit of time.
Flight Speed - (Measured in Meter per Second) - Flight Speed refers to the velocity at which an aircraft moves through the air.

STEP 1: Convert Input(s) to Base Unit

Ideal Thrust: 479.5 Newton --> 479.5 Newton No Conversion Required
Mass Flow Rate: 3.5 Kilogram per Second --> 3.5 Kilogram per Second No Conversion Required
Flight Speed: 111 Meter per Second --> 111 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V_e = T_ideal/m_a+V --> 479.5/3.5+111

Evaluating ... ...

V_e = 248

STEP 3: Convert Result to Output's Unit

248 Meter per Second --> No Conversion Required

FINAL ANSWER

248 Meter per Second <-- Exit Velocity

(Calculation completed in 00.004 seconds)

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Created by Himanshu Sharma

National Institute of Technology, Hamirpur (NITH), Himachal Pradesh

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National Institute Of Technology (NIT), Hamirpur

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< Thrust Generation Calculators

Total Thrust given Efficiency and Enthalpy

LaTeX Go Total Thrust = Mass Flow Rate*((sqrt(2*Enthalpy Drop in Nozzle*Nozzle Efficiency))-Flight Speed+(sqrt(Turbine Efficiency*Efficiency of Transmission*Enthalpy Drop in Turbine)))

Thrust power

LaTeX Go Thrust Power = Mass Flow Rate*Flight Speed*(Exit Velocity-Flight Speed)

Ideal Thrust given Effective Speed Ratio

LaTeX Go Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1)

Specific thrust

LaTeX Go Specific Thrust = Exit Velocity-Flight Speed

Velocity after Expansion given Ideal Thrust Formula

LaTeX Go

Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed
V_e = T_ideal/m_a+V

What is velocity?

Velocity is the directional speed of an object in motion as an indication of its rate of change in position as observed from a particular frame of reference and as measured by a particular standard of time.

How to Calculate Velocity after Expansion given Ideal Thrust?

Velocity after Expansion given Ideal Thrust calculator uses Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed to calculate the Exit Velocity, Velocity after Expansion given Ideal Thrust is a measure of the velocity achieved by an object after expansion, calculated by considering the ideal thrust, mass flow rate, and flight speed of the object, providing valuable insights into the object's motion and behavior. Exit Velocity is denoted by V_e symbol.

How to calculate Velocity after Expansion given Ideal Thrust using this online calculator? To use this online calculator for Velocity after Expansion given Ideal Thrust, enter Ideal Thrust (T_ideal), Mass Flow Rate (m_a) & Flight Speed (V) and hit the calculate button. Here is how the Velocity after Expansion given Ideal Thrust calculation can be explained with given input values -> 240.4286 = 479.5/3.5+111.

FAQ

What is Velocity after Expansion given Ideal Thrust?

Velocity after Expansion given Ideal Thrust is a measure of the velocity achieved by an object after expansion, calculated by considering the ideal thrust, mass flow rate, and flight speed of the object, providing valuable insights into the object's motion and behavior and is represented as V_e = T_ideal/m_a+V or Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed. Ideal Thrust is the thrust produced by an engine when nozzle exit pressure is same as ambient pressure or nozzle is perfectly expanded, Mass Flow Rate represents the amount of mass passing through a system per unit of time & Flight Speed refers to the velocity at which an aircraft moves through the air.

How to calculate Velocity after Expansion given Ideal Thrust?

Velocity after Expansion given Ideal Thrust is a measure of the velocity achieved by an object after expansion, calculated by considering the ideal thrust, mass flow rate, and flight speed of the object, providing valuable insights into the object's motion and behavior is calculated using Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed. To calculate Velocity after Expansion given Ideal Thrust, you need Ideal Thrust (T_ideal), Mass Flow Rate (m_a) & Flight Speed (V). With our tool, you need to enter the respective value for Ideal Thrust, Mass Flow Rate & Flight 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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