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

GoWeight of Aircraft in Level, Unaccelerated Flight Formula

GoWeight of Aircraft for given Coefficients of Lift and Drag Formula

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

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

W_body - Weight of Body?P_dynamic - Dynamic Pressure?A - Area?C_L - Lift Coefficient?

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

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Here is how the Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle equation looks like with Values.

Here is how the Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle equation looks like with Units.

Here is how the Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle equation looks like.

220 = 10 \cdot 20 \cdot 1.1

220N = 10Pa \cdot 20m² \cdot 1.1

220 = 10 \cdot 20 \cdot 1.1

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Aircraft Mechanics » fx Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle

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

Follow our step by step solution on how to calculate Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

W body = 10Pa \cdot 20m² \cdot 1.1

Next Step Prepare to Evaluate

∴

W body = 10 \cdot 20 \cdot 1.1

LAST Step Evaluate

∴

W body = 220N

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

Variables

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

Dynamic Pressure

Dynamic Pressure is a measure of the kinetic energy per unit volume of a fluid in motion.

Symbol: P_dynamic

Measurement: PressureUnit: Pa

Note: Value should be greater than 0.

Formulas to find Dynamic Pressure

Area

The Area is the amount of two-dimensional space taken up by an object.

Symbol: A

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Area

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 Weight of Body

Go Weight of Aircraft in Level, Unaccelerated Flight

W body = F L + (T \cdot \sin (σ T))

Go Weight of Aircraft for given Coefficients of Lift and Drag

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

Go Weight of Aircraft for given Lift-to-Drag Ratio

W body = T \cdot LD

Go Weight of aircraft for given required power

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

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 Thrust Angle for Unaccelerated Level Flight for given Lift

σ T = a \sin (\frac{W body - F L}{T})

Go Thrust of Aircraft required for Level, Unaccelerated Flight

T = P dynamic \cdot A \cdot C D

How to Evaluate Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle?

Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle evaluator uses Weight of Body = Dynamic Pressure*Area*Lift Coefficient to evaluate the Weight of Body, The Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle of the aircraft is balanced by the aerodynamic forces acting on it, at this flight condition, the aircraft is neither climbing nor descending, and its velocity remains constant, negligible thrust angle means that the thrust vector is aligned almost perfectly with the aircraft's longitudinal axis, contributing primarily to forward propulsion rather than vertical lift. Weight of Body is denoted by W_body symbol.

How to evaluate Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle using this online evaluator? To use this online evaluator for Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle, enter Dynamic Pressure (P_dynamic), Area (A) & Lift Coefficient (C_L) and hit the calculate button.

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

What is the formula to find Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle?

The formula of Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle is expressed as Weight of Body = Dynamic Pressure*Area*Lift Coefficient. Here is an example- 88 = 10*20*1.1.

How to calculate Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle?

With Dynamic Pressure (P_dynamic), Area (A) & Lift Coefficient (C_L) we can find Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle using the formula - Weight of Body = Dynamic Pressure*Area*Lift Coefficient.

What are the other ways to Calculate Weight of Body?

Here are the different ways to Calculate Weight of Body-

Weight of Body=Lift Force+(Thrust*sin(Thrust Angle))
Weight of Body=Lift Coefficient*Thrust/Drag Coefficient
Weight of Body=Thrust*Lift-to-Drag Ratio

Can the Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle be negative?

No, the Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle, measured in Force cannot be negative.

Which unit is used to measure Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle?

Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle can be measured.

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

​GoWeight of Aircraft in Level, Unaccelerated Flight Formula

​GoWeight of Aircraft for given Coefficients of Lift and Drag Formula

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

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

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

Other Formulas to find Weight of Body

Other formulas in Thrust and Power Requirements category

How to Evaluate Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle?

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

Variable Name

GoWeight of Aircraft in Level, Unaccelerated Flight Formula

GoWeight of Aircraft for given Coefficients of Lift and Drag Formula