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Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio Formula

GoMean Aerodynamic Chord for given Tail Pitching Moment Coefficient Formula

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The Mean Aerodynamic Chord is a two-dimensional representation of the whole wing. Check FAQs

c ma = 𝒍 t \cdot \frac{S t}{S \cdot V H}

c_ma - Mean Aerodynamic Chord?𝒍_t - Horizontal Tail Moment Arm?S_t - Horizontal Tail Area?S - Reference Area?V_H - Horizontal Tail Volume Ratio?

Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio Example

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Here is how the Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio equation looks like with Values.

Here is how the Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio equation looks like with Units.

Here is how the Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio equation looks like.

0.2 = 0.8015 \cdot \frac{1.8}{5.08 \cdot 1.42}

0.2m = 0.8015m \cdot \frac{1.8m²}{5.08m² \cdot 1.42}

0.2 = 0.8015 \cdot \frac{1.8}{5.08 \cdot 1.42}

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Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio Solution

Follow our step by step solution on how to calculate Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio?

FIRST Step Consider the formula

c ma = 𝒍 t \cdot \frac{S t}{S \cdot V H}

Next Step Substitute values of Variables

∴

c ma = 0.8015m \cdot \frac{1.8m²}{5.08m² \cdot 1.42}

Next Step Prepare to Evaluate

∴

c ma = 0.8015 \cdot \frac{1.8}{5.08 \cdot 1.42}

Next Step Evaluate

∴

c ma = 0.199999972274592m

LAST Step Rounding Answer

∴

c ma = 0.2m

Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio Formula Elements

Variables

Mean Aerodynamic Chord

The Mean Aerodynamic Chord is a two-dimensional representation of the whole wing.

Symbol: c_ma

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Mean Aerodynamic Chord

Horizontal Tail Moment Arm

The Horizontal Tail Moment Arm is the distance between the lift center of the horizontal tail and the center of gravity of the aircraft.

Symbol: 𝒍_t

Measurement: LengthUnit: m

Note: Value can be positive or negative.

Formulas to find Horizontal Tail Moment Arm

Horizontal Tail Area

The Horizontal Tail Area is the surface area of the horizontal stabilizer on an aircraft, which provides pitch stability and control.

Symbol: S_t

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Horizontal Tail Area

Reference Area

The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.

Symbol: S

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Reference Area

Horizontal Tail Volume Ratio

Horizontal Tail Volume Ratio relates the area of the horizontal tail, the distance between tail and aircraft's c.g., the wing area, and the mean aerodynamic wing chord.

Symbol: V_H

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Horizontal Tail Volume Ratio

Other Formulas to find Mean Aerodynamic Chord

Go Mean Aerodynamic Chord for given Tail Pitching Moment Coefficient

c ma = \frac{M t}{0.5 \cdot ρ ∞ \cdot V^{2} \cdot S \cdot Cm t}

Other formulas in Tail Contribution category

Go Tail Pitching Moment for given Lift Coefficient

M t = - \frac{𝒍 t \cdot CT lift \cdot ρ ∞ \cdot {V tail}^{2} \cdot S t}{2}

Go Tail Lift for given Tail Pitching Moment

L t = - (\frac{M t}{𝒍 t})

Go Pitching Moment due to Tail

M t = - 𝒍 t \cdot L t

Go Tail Pitching Moment for given Moment Coefficient

M t = \frac{Cm t \cdot ρ ∞ \cdot V^{2} \cdot S \cdot c ma}{2}

How to Evaluate Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio?

Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio evaluator uses Mean Aerodynamic Chord = Horizontal Tail Moment Arm*Horizontal Tail Area/(Reference Area*Horizontal Tail Volume Ratio) to evaluate the Mean Aerodynamic Chord, Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio is a measure of the average distance from the root to the tip of a wing, calculated in relation to the horizontal tail's volume ratio, area, and moment arm, providing a vital parameter for aircraft design and stability analysis. Mean Aerodynamic Chord is denoted by c_ma symbol.

How to evaluate Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio using this online evaluator? To use this online evaluator for Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio, enter Horizontal Tail Moment Arm (𝒍_t), Horizontal Tail Area (S_t), Reference Area (S) & Horizontal Tail Volume Ratio (V_H) and hit the calculate button.

FAQs on Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio

What is the formula to find Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio?

The formula of Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio is expressed as Mean Aerodynamic Chord = Horizontal Tail Moment Arm*Horizontal Tail Area/(Reference Area*Horizontal Tail Volume Ratio). Here is an example- 0.2 = 0.801511*1.8/(5.08*1.42).

How to calculate Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio?

With Horizontal Tail Moment Arm (𝒍_t), Horizontal Tail Area (S_t), Reference Area (S) & Horizontal Tail Volume Ratio (V_H) we can find Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio using the formula - Mean Aerodynamic Chord = Horizontal Tail Moment Arm*Horizontal Tail Area/(Reference Area*Horizontal Tail Volume Ratio).

What are the other ways to Calculate Mean Aerodynamic Chord?

Here are the different ways to Calculate Mean Aerodynamic Chord-

Mean Aerodynamic Chord=Pitching Moment due to Tail/(0.5*Freestream Density*Flight Velocity^2*Reference Area*Tail Pitching Moment Coefficient)

Can the Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio be negative?

No, the Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio, measured in Length cannot be negative.

Which unit is used to measure Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio?

Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio is usually measured using the Meter[m] for Length. Millimeter[m], Kilometer[m], Decimeter[m] are the few other units in which Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio can be measured.

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Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio Formula

​GoMean Aerodynamic Chord for given Tail Pitching Moment Coefficient Formula

Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio Example

Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio Solution

Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio Formula Elements

Other Formulas to find Mean Aerodynamic Chord

Other formulas in Tail Contribution category

How to Evaluate Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio?

FAQs on Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio

Variable Name

GoMean Aerodynamic Chord for given Tail Pitching Moment Coefficient Formula