Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 200+ more calculators!
Vaibhav Malani
National Institute of Technology (NIT), Tiruchirapalli
Vaibhav Malani has verified this Calculator and 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Total thrust if efficiency and enthalpy is known
Total thrust=Air flow rate*((sqrt(2*Enthalpy drop in nozzle*Efficiency of nozzle))-Aircraft forward speed+(sqrt(Efficiency of turbine*Transmission efficiency of propeller*Enthalpy drop in turbine))) GO
Propulsive power
Propulsive power=1/2*((Air flow rate+Fuel flow rate)*Jet velocity of aircraft^2-(Air flow rate*Aircraft forward speed^2)) GO
Thermal efficiency of jet engines if effective speed ratio is known
Thermal efficiency=Jet velocity of aircraft^2*(1-Effective speed ratio^2)/(2*Fuel air ratio*Calorific value of fuel) GO
Thrust power
Thrust power=Air flow rate*Aircraft forward speed*(Jet velocity of aircraft-Aircraft forward speed) GO
Kinetic energy of gases at exit
Kinetic Energy=1/2*Mass Flow Rate*(1+Air to Fuel Ratio)*Jet velocity of aircraft^2 GO
Thrust if effective speed ratio is known
Thrust=Air flow rate*Aircraft forward speed*((1/Effective speed ratio)-1) GO
Thrust if aircraft forward speed, velocity of exhaust is known
Thrust=Air flow rate*(Jet velocity of aircraft-Aircraft forward speed) GO
Effective speed ratio
Effective speed ratio=Aircraft forward speed/Jet velocity of aircraft GO
specific thrust if effective speed ratio is known
Specific thrust=Jet velocity of aircraft*(1-Effective speed ratio) GO
Specific thrust
Specific thrust=Jet velocity of aircraft-Aircraft forward speed GO
Kinetic energy of air at inlet
Kinetic Energy=1/2*Air flow rate*Aircraft forward speed^2 GO

Gross thrust Formula

Gross thrust=Air flow rate*Jet velocity of aircraft
T=m<sub>a</sub>*C<sub>j</sub>
More formulas
Total thrust if nozzle thrust and propeller thrust is known GO
Total thrust if efficiency and enthalpy is known GO
Thrust if aircraft forward speed, velocity of exhaust is known GO
Thrust if effective speed ratio is known GO
Thrust power GO
Specific thrust GO
specific thrust if effective speed ratio is known GO
Jet velocity if enthalpy drop is known GO
Jet velocity if temperature drop is known GO
Thermal efficiency of turbojet engine GO
Propulsive power GO
Thermal efficiency of jet engines if effective speed ratio is known GO
Thermal efficiency of propeller engines GO
Propeller Efficiency GO
Transmission Efficiency GO
Thrust specific fuel consumption GO
Kinetic energy of air at inlet GO
Kinetic energy of gases at exit GO
Propulsive efficiency GO
Propulsive efficiency if effective speed ratio is known GO
Effective speed ratio GO
Inlet drag GO
Propulsive efficiency if aircraft velocity is known GO
Overall efficiency of a propulsive system GO
Thrust power specific fuel consumption GO
Momentum thrust GO
Propeller efficiency if thrust is known GO

What is gross thrust?

Gross thrust is the total thrust of a jet engine without deduction of the drag caused by the momentum of the incoming air. It is also given as the product of mass flow rate of air and the aircraft jet velocity.

How to Calculate Gross thrust?

Gross thrust calculator uses Gross thrust=Air flow rate*Jet velocity of aircraft to calculate the Gross thrust, The Gross thrust formula is defined as the product of mass flow rate of air and the aircraft jet velocity. Gross thrust and is denoted by T symbol.

How to calculate Gross thrust using this online calculator? To use this online calculator for Gross thrust, enter Air flow rate (ma) and Jet velocity of aircraft (Cj) and hit the calculate button. Here is how the Gross thrust calculation can be explained with given input values -> 744 = 3*248.

FAQ

What is Gross thrust?
The Gross thrust formula is defined as the product of mass flow rate of air and the aircraft jet velocity and is represented as T=ma*Cj or Gross thrust=Air flow rate*Jet velocity of aircraft. Air flow rate is the mass flow rate of air and Jet velocity of aircraft is the velocity of exhaust from aircraft.
How to calculate Gross thrust?
The Gross thrust formula is defined as the product of mass flow rate of air and the aircraft jet velocity is calculated using Gross thrust=Air flow rate*Jet velocity of aircraft. To calculate Gross thrust, you need Air flow rate (ma) and Jet velocity of aircraft (Cj). With our tool, you need to enter the respective value for Air flow rate and Jet velocity of aircraft 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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