Total thrust given nozzle thrust and propeller thrust Calculator

↳

⤿

Jet Propulsion

Components of Gas Turbine

Rocket Propulsion

Thermodynamics and Governing Equations

⤿

Turboprops

Performance Parameters

Turbofans

Turbojets

Turbomachinery Equations

✖Nozzle thrust is the thrust produced by the nozzle.ⓘ Nozzle Thrust [T_nozzle]			+10% -10%
✖Propeller Thrust is the force generated by a rotating propeller, driving an aircraft forward.ⓘ Propeller Thrust [T_prop]			+10% -10%

✖Total thrust is the sum of nozzle and propeller thrust.ⓘ Total thrust given nozzle thrust and propeller thrust [T]

⎘ Copy

👎

Formula

✖

Total thrust given nozzle thrust and propeller thrust

Formula

`"T" = "T"_{"nozzle"}+"T"_{"prop"}`

Example

`"1.71kN"="0.5kN"+"1.21kN"`

Calculator

LaTeX

Reset

👍

Download Aeroengines Formula PDF

Total thrust given nozzle thrust and propeller thrust Solution

STEP 0: Pre-Calculation Summary

Formula Used

Total Thrust = Nozzle Thrust+Propeller Thrust
T = T_nozzle+T_prop
This formula uses 3 Variables

Variables Used

Total Thrust - (Measured in Newton) - Total thrust is the sum of nozzle and propeller thrust.
Nozzle Thrust - (Measured in Newton) - Nozzle thrust is the thrust produced by the nozzle.
Propeller Thrust - (Measured in Newton) - Propeller Thrust is the force generated by a rotating propeller, driving an aircraft forward.

STEP 1: Convert Input(s) to Base Unit

Nozzle Thrust: 0.5 Kilonewton --> 500 Newton (Check conversion here)
Propeller Thrust: 1.21 Kilonewton --> 1210 Newton (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

T = T_nozzle+T_prop --> 500+1210

Evaluating ... ...

T = 1710

STEP 3: Convert Result to Output's Unit

1710 Newton -->1.71 Kilonewton (Check conversion here)

FINAL ANSWER

1.71 Kilonewton <-- Total Thrust

(Calculation completed in 00.004 seconds)

You are here -

Home » Physics » Aeroengines » Jet Propulsion » Turboprops » Total thrust given nozzle thrust and propeller thrust

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!

< 4 Turboprops Calculators

Thermal Efficiency of Propeller Engines

Go Thermal Efficiency = Break Power/(Fuel Flow Rate*Fuel Calorific Value)

Propeller efficiency given thrust

Go Propeller Efficiency = (Propeller Thrust*Flight Speed)/Shaft Power

Propeller Efficiency

Go Propeller Efficiency = Thrust Power/Shaft Power

Total thrust given nozzle thrust and propeller thrust

Go Total Thrust = Nozzle Thrust+Propeller Thrust

Total thrust given nozzle thrust and propeller thrust Formula

Total Thrust = Nozzle Thrust+Propeller Thrust
T = T_nozzle+T_prop

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 Total thrust given nozzle thrust and propeller thrust?

Total thrust given nozzle thrust and propeller thrust calculator uses Total Thrust = Nozzle Thrust+Propeller Thrust to calculate the Total Thrust, The Total thrust given nozzle thrust and propeller thrust formula is defined as the sum of nozzle thrust and propeller thrust. Total Thrust is denoted by T symbol.

How to calculate Total thrust given nozzle thrust and propeller thrust using this online calculator? To use this online calculator for Total thrust given nozzle thrust and propeller thrust, enter Nozzle Thrust (T_nozzle) & Propeller Thrust (T_prop) and hit the calculate button. Here is how the Total thrust given nozzle thrust and propeller thrust calculation can be explained with given input values -> 0.001255 = 500+1210.

FAQ

What is Total thrust given nozzle thrust and propeller thrust?

The Total thrust given nozzle thrust and propeller thrust formula is defined as the sum of nozzle thrust and propeller thrust and is represented as T = T_nozzle+T_prop or Total Thrust = Nozzle Thrust+Propeller Thrust. Nozzle thrust is the thrust produced by the nozzle & Propeller Thrust is the force generated by a rotating propeller, driving an aircraft forward.

How to calculate Total thrust given nozzle thrust and propeller thrust?

The Total thrust given nozzle thrust and propeller thrust formula is defined as the sum of nozzle thrust and propeller thrust is calculated using Total Thrust = Nozzle Thrust+Propeller Thrust. To calculate Total thrust given nozzle thrust and propeller thrust, you need Nozzle Thrust (T_nozzle) & Propeller Thrust (T_prop). With our tool, you need to enter the respective value for Nozzle Thrust & Propeller Thrust and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

Home

FREE PDFs

🔍 Search