Thrust available for given excess power Calculator

✖Drag Force is the resisting force experienced by an object moving through a fluid.ⓘ Drag Force [F_D]			+10% -10%
✖Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft.ⓘ Excess Power [P_excess]			+10% -10%
✖Velocity is a vector quantity (it has both magnitude and direction) and is the rate of change of the position of an object with respect to time.ⓘ Velocity [v]			+10% -10%

✖Thrust denotes the force exerted by the engine to propel an aircraft forward.ⓘ Thrust available for given excess power [T]

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Thrust available for given excess power Solution

STEP 0: Pre-Calculation Summary

Formula Used

Thrust = Drag Force+(Excess Power/Velocity)
T = F_D+(P_excess/v)
This formula uses 4 Variables

Variables Used

Thrust - (Measured in Newton) - Thrust denotes the force exerted by the engine to propel an aircraft forward.
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid.
Excess Power - (Measured in Watt) - Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft.
Velocity - (Measured in Meter per Second) - Velocity is a vector quantity (it has both magnitude and direction) and is the rate of change of the position of an object with respect to time.

STEP 1: Convert Input(s) to Base Unit

Drag Force: 80.04 Newton --> 80.04 Newton No Conversion Required
Excess Power: 37197.6 Watt --> 37197.6 Watt No Conversion Required
Velocity: 60 Meter per Second --> 60 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

T = F_D+(P_excess/v) --> 80.04+(37197.6/60)

Evaluating ... ...

T = 700

STEP 3: Convert Result to Output's Unit

700 Newton --> No Conversion Required

FINAL ANSWER

700 Newton <-- Thrust

(Calculation completed in 00.004 seconds)

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Credits

Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

Maiarutselvan V has verified this Calculator and 300+ more calculators!

< Climbing Flight Calculators

Flight path angle at given rate of climb

LaTeX Go Flight Path Angle = asin(Rate of Climb/Velocity)

Velocity of aircraft at given rate of climb

LaTeX Go Velocity = Rate of Climb/sin(Flight Path Angle)

Rate of Climb

LaTeX Go Rate of Climb = Velocity*sin(Flight Path Angle)

Weight of Aircraft for given Excess Power

LaTeX Go Aircraft Weight = Excess Power/Rate of Climb

Thrust available for given excess power Formula

LaTeX Go

Thrust = Drag Force+(Excess Power/Velocity)
T = F_D+(P_excess/v)

How is excess thrust desirable?

Airplanes with a high excess thrust, like fighter planes, can accelerate faster than aircraft with low excess thrust.

How to Calculate Thrust available for given excess power?

Thrust available for given excess power calculator uses Thrust = Drag Force+(Excess Power/Velocity) to calculate the Thrust, The Thrust available for given excess power can be calculated by considering the relationship between power and thrust, thrust required during climb flight is the sum of the drag force and the additional thrust needed to compensate for the excess power available. Thrust is denoted by T symbol.

How to calculate Thrust available for given excess power using this online calculator? To use this online calculator for Thrust available for given excess power, enter Drag Force (F_D), Excess Power (P_excess) & Velocity (v) and hit the calculate button. Here is how the Thrust available for given excess power calculation can be explained with given input values -> 700.03 = 80.04+(37197.6/60).

FAQ

What is Thrust available for given excess power?

The Thrust available for given excess power can be calculated by considering the relationship between power and thrust, thrust required during climb flight is the sum of the drag force and the additional thrust needed to compensate for the excess power available and is represented as T = F_D+(P_excess/v) or Thrust = Drag Force+(Excess Power/Velocity). Drag Force is the resisting force experienced by an object moving through a fluid, Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft & Velocity is a vector quantity (it has both magnitude and direction) and is the rate of change of the position of an object with respect to time.

How to calculate Thrust available for given excess power?

The Thrust available for given excess power can be calculated by considering the relationship between power and thrust, thrust required during climb flight is the sum of the drag force and the additional thrust needed to compensate for the excess power available is calculated using Thrust = Drag Force+(Excess Power/Velocity). To calculate Thrust available for given excess power, you need Drag Force (F_D), Excess Power (P_excess) & Velocity (v). With our tool, you need to enter the respective value for Drag Force, Excess Power & Velocity 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 Thrust?

In this formula, Thrust uses Drag Force, Excess Power & Velocity. We can use 1 other way(s) to calculate the same, which is/are as follows -

Thrust = (sec(Thrust Angle))*(Drag Force+(Mass of Aircraft*[g]*sin(Flight Path Angle))+(Mass of Aircraft*Acceleration))

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