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Thrust for given coefficients of lift and drag Formula

GoThrust for Level and Unaccelerated Flight Formula

GoThrust of Aircraft required for Level, Unaccelerated Flight Formula

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

T = C D \cdot \frac{W body}{C L}

T - Thrust?C_D - Drag Coefficient?W_body - Weight of Body?C_L - Lift Coefficient?

Thrust for given coefficients of lift and drag Example

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Here is how the Thrust for given coefficients of lift and drag equation looks like with Values.

Here is how the Thrust for given coefficients of lift and drag equation looks like with Units.

Here is how the Thrust for given coefficients of lift and drag equation looks like.

100.4545 = 0.5 \cdot \frac{221}{1.1}

100.4545N = 0.5 \cdot \frac{221N}{1.1}

100.4545 = 0.5 \cdot \frac{221}{1.1}

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Thrust for given coefficients of lift and drag Solution

Follow our step by step solution on how to calculate Thrust for given coefficients of lift and drag?

FIRST Step Consider the formula

T = C D \cdot \frac{W body}{C L}

Next Step Substitute values of Variables

∴

T = 0.5 \cdot \frac{221N}{1.1}

Next Step Prepare to Evaluate

∴

T = 0.5 \cdot \frac{221}{1.1}

Next Step Evaluate

∴

T = 100.454545454545N

LAST Step Rounding Answer

∴

T = 100.4545N

Thrust for given coefficients of lift and drag Formula Elements

Variables

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

Drag Coefficient

Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.

Symbol: C_D

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Drag Coefficient

Weight of Body

Weight of Body is the force acting on the object due to gravity.

Symbol: W_body

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Weight of Body

Lift Coefficient

The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

Symbol: C_L

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Lift Coefficient

Other Formulas to find Thrust

Go Thrust for Level and Unaccelerated Flight

T = \frac{F D}{\cos (σ T)}

Go Thrust of Aircraft required for Level, Unaccelerated Flight

T = P dynamic \cdot A \cdot C D

Go Thrust of aircraft required for given Lift-to-drag ratio

T = \frac{W body}{LD}

Go Minimum Thrust of aircraft required

T = P dynamic \cdot S \cdot (C D,0 + C D,i)

Other formulas in Thrust and Power Requirements category

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})

Go Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle

W body = P dynamic \cdot A \cdot C L

How to Evaluate Thrust for given coefficients of lift and drag?

Thrust for given coefficients of lift and drag evaluator uses Thrust = Drag Coefficient*Weight of Body/Lift Coefficient to evaluate the Thrust, The Thrust for given coefficients of lift and drag is the amount of propulsive force needed to maintain level flight while producing the specified lift and overcoming aerodynamic drag, in level flight, the thrust required is equal to the drag experienced by the aircraft, the drag force is determined by the aerodynamic coefficients of lift and drag, as well as other factors such as air density, velocity, and reference area. Thrust is denoted by T symbol.

How to evaluate Thrust for given coefficients of lift and drag using this online evaluator? To use this online evaluator for Thrust for given coefficients of lift and drag, enter Drag Coefficient (C_D), Weight of Body (W_body) & Lift Coefficient (C_L) and hit the calculate button.

FAQs on Thrust for given coefficients of lift and drag

What is the formula to find Thrust for given coefficients of lift and drag?

The formula of Thrust for given coefficients of lift and drag is expressed as Thrust = Drag Coefficient*Weight of Body/Lift Coefficient. Here is an example- 6027.273 = 0.5*221/1.1.

How to calculate Thrust for given coefficients of lift and drag?

With Drag Coefficient (C_D), Weight of Body (W_body) & Lift Coefficient (C_L) we can find Thrust for given coefficients of lift and drag using the formula - Thrust = Drag Coefficient*Weight of Body/Lift Coefficient.

What are the other ways to Calculate Thrust?

Here are the different ways to Calculate Thrust-

Thrust=Drag Force/(cos(Thrust Angle))
Thrust=Dynamic Pressure*Area*Drag Coefficient
Thrust=Weight of Body/Lift-to-Drag Ratio

Can the Thrust for given coefficients of lift and drag be negative?

No, the Thrust for given coefficients of lift and drag, measured in Force cannot be negative.

Which unit is used to measure Thrust for given coefficients of lift and drag?

Thrust for given coefficients of lift and drag is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Thrust for given coefficients of lift and drag can be measured.

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Thrust for given coefficients of lift and drag Formula

​GoThrust for Level and Unaccelerated Flight Formula

​GoThrust of Aircraft required for Level, Unaccelerated Flight Formula

Thrust for given coefficients of lift and drag Example

Thrust for given coefficients of lift and drag Solution

Thrust for given coefficients of lift and drag Formula Elements

Other Formulas to find Thrust

Other formulas in Thrust and Power Requirements category

How to Evaluate Thrust for given coefficients of lift and drag?

FAQs on Thrust for given coefficients of lift and drag

Variable Name

GoThrust for Level and Unaccelerated Flight Formula

GoThrust of Aircraft required for Level, Unaccelerated Flight Formula