Ideal Thrust given Effective Speed Ratio Calculator

✖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]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Thrust Generation Formulas PDF PDF Image

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)

You are here -

Home » Physics » Propulsion » Jet Propulsion » Performance Parameters » Aerospace » Thrust Generation » Ideal Thrust given Effective Speed Ratio

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 Vaibhav Malani

National Institute of Technology (NIT), Tiruchirapalli

Vaibhav Malani has verified this Calculator and 200+ more calculators!

< 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

Ideal Thrust given Effective Speed Ratio Formula

LaTeX Go

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 a measure of the thrust produced by an aircraft or a jet engine, calculated by considering the mass flow rate, flight speed, and effective speed ratio, providing a crucial parameter for aerodynamic analysis and aircraft design. 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 a measure of the thrust produced by an aircraft or a jet engine, calculated by considering the mass flow rate, flight speed, and effective speed ratio, providing a crucial parameter for aerodynamic analysis and aircraft design 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 a measure of the thrust produced by an aircraft or a jet engine, calculated by considering the mass flow rate, flight speed, and effective speed ratio, providing a crucial parameter for aerodynamic analysis and aircraft design 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)

Home

FREE PDFs

🔍 Search