FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Power required for given required thrust of aircraft Formula

GoPower required for given aerodynamic coefficients Formula

GoPower required for given total drag force Formula

Fx Copy

LaTeX Copy

Power is defined as the product of thrust force and velocity of aircraft. Check FAQs

P = V ∞ \cdot T

P - Power?V_∞ - Freestream Velocity?T - Thrust?

Power required for given required thrust of aircraft Example

With values

With units

Only example

Here is how the Power required for given required thrust of aircraft equation looks like with Values.

Here is how the Power required for given required thrust of aircraft equation looks like with Units.

Here is how the Power required for given required thrust of aircraft equation looks like.

3000 = 30 \cdot 100

3000W = 30m/s \cdot 100N

3000 = 30 \cdot 100

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Aerospace » Category

Aircraft Mechanics » fx Power required for given required thrust of aircraft

Power required for given required thrust of aircraft Solution

Follow our step by step solution on how to calculate Power required for given required thrust of aircraft?

FIRST Step Consider the formula

P = V ∞ \cdot T

Next Step Substitute values of Variables

∴

P = 30m/s \cdot 100N

Next Step Prepare to Evaluate

∴

P = 30 \cdot 100

LAST Step Evaluate

∴

P = 3000W

Power required for given required thrust of aircraft Formula Elements

Variables

Power

Power is defined as the product of thrust force and velocity of aircraft.

Symbol: P

Measurement: PowerUnit: W

Note: Value should be greater than 0.

Formulas to find Power

Freestream Velocity

The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air.

Symbol: V_∞

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Freestream Velocity

Thrust

The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air.

Symbol: T

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Thrust

Other Formulas to find Power

Go Power required for given aerodynamic coefficients

P = W body \cdot V ∞ \cdot \frac{C D}{C L}

Go Power required for given total drag force

P = F D \cdot V ∞

Other formulas in Thrust and Power Requirements category

Go Thrust for Level and Unaccelerated Flight

T = \frac{F D}{\cos (σ T)}

Go Thrust Angle for Unaccelerated Level Flight for given Drag

σ T = a \cos (\frac{F D}{T})

Go Weight of Aircraft in Level, Unaccelerated Flight

W body = F L + (T \cdot \sin (σ T))

Go Thrust Angle for Unaccelerated Level Flight for given Lift

σ T = a \sin (\frac{W body - F L}{T})

How to Evaluate Power required for given required thrust of aircraft?

Power required for given required thrust of aircraft evaluator uses Power = Freestream Velocity*Thrust to evaluate the Power, The Power required for given required thrust of aircraft represents the amount of power necessary to sustain level flight while producing the specified thrust, in aerodynamics, this concept is crucial for understanding the energy demands of an aircraft's propulsion system, the power required for level flight is directly related to the thrust generated by the aircraft's engines and its velocity. Power is denoted by P symbol.

How to evaluate Power required for given required thrust of aircraft using this online evaluator? To use this online evaluator for Power required for given required thrust of aircraft, enter Freestream Velocity (V_∞) & Thrust (T) and hit the calculate button.

FAQs on Power required for given required thrust of aircraft

What is the formula to find Power required for given required thrust of aircraft?

The formula of Power required for given required thrust of aircraft is expressed as Power = Freestream Velocity*Thrust. Here is an example- 3000 = 30*100.

How to calculate Power required for given required thrust of aircraft?

With Freestream Velocity (V_∞) & Thrust (T) we can find Power required for given required thrust of aircraft using the formula - Power = Freestream Velocity*Thrust.

What are the other ways to Calculate Power?

Here are the different ways to Calculate Power-

Power=Weight of Body*Freestream Velocity*Drag Coefficient/Lift Coefficient
Power=Drag Force*Freestream Velocity

Can the Power required for given required thrust of aircraft be negative?

No, the Power required for given required thrust of aircraft, measured in Power cannot be negative.

Which unit is used to measure Power required for given required thrust of aircraft?

Power required for given required thrust of aircraft is usually measured using the Watt[W] for Power. Kilowatt[W], Milliwatt[W], Microwatt[W] are the few other units in which Power required for given required thrust of aircraft can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Power required for given required thrust of aircraft Formula

​GoPower required for given aerodynamic coefficients Formula

​GoPower required for given total drag force Formula

Power required for given required thrust of aircraft Example

Power required for given required thrust of aircraft Solution

Power required for given required thrust of aircraft Formula Elements

Other Formulas to find Power

Other formulas in Thrust and Power Requirements category

How to Evaluate Power required for given required thrust of aircraft?

FAQs on Power required for given required thrust of aircraft

Variable Name

GoPower required for given aerodynamic coefficients Formula

GoPower required for given total drag force Formula