Ideal Thrust given Effective Speed Ratio Calculator

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Thrust Generation

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✖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%
✖Effective speed ratio is the ratio of aircraft forward speed to the aircraft jet velocity.ⓘ Effective Speed Ratio [α]			+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 given Effective Speed Ratio [T_ideal]

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Formula

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Ideal Thrust given Effective Speed Ratio

Formula

`"T"_{"ideal"} = "m"_{"a"}*"V"*((1/"α")-1)`

Example

`"479.6564N"="3.5kg/s"*"111m/s"*((1/"0.4475")-1)`

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Ideal Thrust given Effective Speed Ratio Solution

STEP 0: Pre-Calculation Summary

Formula Used

Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1)
T_ideal = m_a*V*((1/α)-1)
This formula uses 4 Variables

Variables Used

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.
Effective Speed Ratio - Effective speed ratio is the ratio of aircraft forward speed to the aircraft jet velocity.

STEP 1: Convert Input(s) to Base Unit

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
Effective Speed Ratio: 0.4475 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

T_ideal = m_a*V*((1/α)-1) --> 3.5*111*((1/0.4475)-1)

Evaluating ... ...

T_ideal = 479.656424581006

STEP 3: Convert Result to Output's Unit

479.656424581006 Newton --> No Conversion Required

FINAL ANSWER

479.656424581006 ≈ 479.6564 Newton <-- Ideal Thrust

(Calculation completed in 00.004 seconds)

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Created by Chilvera Bhanu Teja

Institute of Aeronautical Engineering (IARE), Hyderabad

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< 21 Thrust Generation Calculators

Total Thrust given Efficiency and Enthalpy

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)))

Momentum Thrust

Go Ideal Thrust = Mass Flow Rate*((1+Fuel Air Ratio)*Exit Velocity-Flight Speed)

Thrust power

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

Ideal Thrust given Effective Speed Ratio

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

Thrust given aircraft forward speed, velocity of exhaust

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

Mass Flow Rate given Ideal Thrust

Go Mass Flow Rate = Ideal Thrust/(Exit Velocity-Flight Speed)

Ideal Thrust of Jet Engine

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

Velocity after Expansion given Ideal Thrust

Go Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed

Flight Speed given Ideal Thrust

Go Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate

Thrust specific fuel consumption

Go Thrust-Specific Fuel Consumption = (3600*Fuel Air Ratio)/Specific Thrust

Thrust power specific fuel consumption

Go Thrust Power Specific Fuel Consumption = Fuel Flow Rate/Thrust Power

Gross Thrust Coefficient

Go Gross Thrust Coefficient = Gross Thrust/Ideal Gross Thrust

Specific Thrust given Effective Speed Ratio

Go Specific Thrust = Exit Velocity*(1-Effective Speed Ratio)

Flight Speed given Momentum of Ambient Air

Go Flight Speed = Momentum of Ambient Air/Mass Flow Rate

Mass Flow given Momentum in Ambient Air

Go Mass Flow Rate = Momentum of Ambient Air/Flight Speed

Momentum of Ambient Air

Go Momentum of Ambient Air = Mass Flow Rate*Flight Speed

Specific thrust

Go Specific Thrust = Exit Velocity-Flight Speed

Gross thrust

Go Gross Thrust = Mass Flow Rate*Exit Velocity

Mass Flow Rate given Ram Drag and Flight Speed

Go Mass Flow Rate = Ram Drag/Flight Speed

Flight Speed given Ram Drag and Mass Flow Rate

Go Flight Speed = Ram Drag/Mass Flow Rate

Ram drag

Go Ram Drag = Mass Flow Rate*Flight Speed

Ideal Thrust given Effective Speed Ratio Formula

Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1)
T_ideal = m_a*V*((1/α)-1)

What is thrust?

Thrust is the force which moves an aircraft through the air. Thrust is used to overcome the drag of an airplane, and to overcome the weight of a rocket.

How to Calculate Ideal Thrust given Effective Speed Ratio?

Ideal Thrust given Effective Speed Ratio calculator uses Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1) to calculate the Ideal Thrust, Ideal Thrust given Effective Speed Ratio is defined as the product of mass flow rate of air and aircraft forward speed and multiplied by difference between reciprocal of effective speed ratio and one. Ideal Thrust is denoted by T_ideal symbol.

How to calculate Ideal Thrust given Effective Speed Ratio using this online calculator? To use this online calculator for Ideal Thrust given Effective Speed Ratio, enter Mass Flow Rate (m_a), Flight Speed (V) & Effective Speed Ratio (α) and hit the calculate button. Here is how the Ideal Thrust given Effective Speed Ratio calculation can be explained with given input values -> 494.4545 = 3.5*111*((1/0.4475)-1).

FAQ

What is Ideal Thrust given Effective Speed Ratio?

Ideal Thrust given Effective Speed Ratio is defined as the product of mass flow rate of air and aircraft forward speed and multiplied by difference between reciprocal of effective speed ratio and one and is represented as T_ideal = m_a*V*((1/α)-1) or Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1). 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 & Effective speed ratio is the ratio of aircraft forward speed to the aircraft jet velocity.

How to calculate Ideal Thrust given Effective Speed Ratio?

Ideal Thrust given Effective Speed Ratio is defined as the product of mass flow rate of air and aircraft forward speed and multiplied by difference between reciprocal of effective speed ratio and one is calculated using Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1). To calculate Ideal Thrust given Effective Speed Ratio, you need Mass Flow Rate (m_a), Flight Speed (V) & Effective Speed Ratio (α). With our tool, you need to enter the respective value for Mass Flow Rate, Flight Speed & Effective Speed Ratio 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 Ideal Thrust?

In this formula, Ideal Thrust uses Mass Flow Rate, Flight Speed & Effective Speed Ratio. We can use 3 other way(s) to calculate the same, which is/are as follows -

Ideal Thrust = Mass Flow Rate*((1+Fuel Air Ratio)*Exit Velocity-Flight Speed)
Ideal Thrust = Mass Flow Rate*(Exit Velocity-Flight Speed)
Ideal Thrust = Mass Flow Rate*(Exit Velocity-Flight Speed)

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