Flight Speed given Ideal Thrust Calculator

✖Exit Velocity refers to the speed at which gases expand at the exit of nozzle of a engine.ⓘ Exit Velocity [V_e]			+10% -10%
✖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 given Ideal Thrust [V]

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Flight Speed given Ideal Thrust Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

Flight Speed - (Measured in Meter per Second) - Flight Speed refers to the velocity at which an aircraft moves through the air.
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.

STEP 1: Convert Input(s) to Base Unit

Exit Velocity: 248 Meter per Second --> 248 Meter per Second No Conversion Required
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

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V = V_e-T_ideal/m_a --> 248-479.5/3.5

Evaluating ... ...

V = 111

STEP 3: Convert Result to Output's Unit

111 Meter per Second --> No Conversion Required

FINAL ANSWER

111 Meter per Second <-- Flight Speed

(Calculation completed in 00.020 seconds)

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Created by Himanshu Sharma

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

Himanshu Sharma has created this Calculator and 50+ more calculators!

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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

Flight Speed given Ideal Thrust Formula

LaTeX Go

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

What is flight speed?

In aviation, V-speeds are standard terms used to define airspeeds important or useful to the operation of all aircraft. These speeds are derived from data obtained by aircraft designers and manufacturers during flight testing for aircraft type-certification.

How to Calculate Flight Speed given Ideal Thrust?

Flight Speed given Ideal Thrust calculator uses Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate to calculate the Flight Speed, Flight Speed given Ideal Thrust is a measure of an aircraft's forward velocity, calculated by considering the ideal thrust, the exit velocity and the mass flow rate, providing a crucial parameter for aircraft performance evaluation and optimization. Flight Speed is denoted by V symbol.

How to calculate Flight Speed given Ideal Thrust using this online calculator? To use this online calculator for Flight Speed given Ideal Thrust, enter Exit Velocity (V_e), Ideal Thrust (T_ideal) & Mass Flow Rate (m_a) and hit the calculate button. Here is how the Flight Speed given Ideal Thrust calculation can be explained with given input values -> 118.5714 = 248-479.5/3.5.

FAQ

What is Flight Speed given Ideal Thrust?

Flight Speed given Ideal Thrust is a measure of an aircraft's forward velocity, calculated by considering the ideal thrust, the exit velocity and the mass flow rate, providing a crucial parameter for aircraft performance evaluation and optimization and is represented as V = V_e-T_ideal/m_a or Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate. Exit Velocity refers to the speed at which gases expand at the exit of nozzle of a engine, 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.

How to calculate Flight Speed given Ideal Thrust?

Flight Speed given Ideal Thrust is a measure of an aircraft's forward velocity, calculated by considering the ideal thrust, the exit velocity and the mass flow rate, providing a crucial parameter for aircraft performance evaluation and optimization is calculated using Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate. To calculate Flight Speed given Ideal Thrust, you need Exit Velocity (V_e), Ideal Thrust (T_ideal) & Mass Flow Rate (m_a). With our tool, you need to enter the respective value for Exit Velocity, Ideal Thrust & Mass Flow Rate 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 Flight Speed?

In this formula, Flight Speed uses Exit Velocity, Ideal Thrust & Mass Flow Rate. We can use 2 other way(s) to calculate the same, which is/are as follows -

Flight Speed = Momentum of Ambient Air/Mass Flow Rate
Flight Speed = Ram Drag/Mass Flow Rate

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