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Mean Aerodynamic Chord for Propeller-Driven Airplane Formula

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

c ma = (\frac{1}{S}) \cdot \int ({L c}^{2}, x, - \frac{b}{2}, \frac{b}{2})

c_ma - Mean Aerodynamic Chord?S - Reference Area?L_c - Chord Length?b - Wingspan?

Mean Aerodynamic Chord for Propeller-Driven Airplane Example

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Here is how the Mean Aerodynamic Chord for Propeller-Driven Airplane equation looks like with Values.

Here is how the Mean Aerodynamic Chord for Propeller-Driven Airplane equation looks like with Units.

Here is how the Mean Aerodynamic Chord for Propeller-Driven Airplane equation looks like.

142.126 = (\frac{1}{5.08}) \cdot \int ({3.8}^{2}, x, - \frac{50}{2}, \frac{50}{2})

142.126m = (\frac{1}{5.08m²}) \cdot \int ({3.8m}^{2}, x, - \frac{50m}{2}, \frac{50m}{2})

142.126 = (\frac{1}{5.08}) \cdot \int ({3.8}^{2}, x, - \frac{50}{2}, \frac{50}{2})

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Mean Aerodynamic Chord for Propeller-Driven Airplane Solution

Follow our step by step solution on how to calculate Mean Aerodynamic Chord for Propeller-Driven Airplane?

FIRST Step Consider the formula

c ma = (\frac{1}{S}) \cdot \int ({L c}^{2}, x, - \frac{b}{2}, \frac{b}{2})

Next Step Substitute values of Variables

∴

c ma = (\frac{1}{5.08m²}) \cdot \int ({3.8m}^{2}, x, - \frac{50m}{2}, \frac{50m}{2})

Next Step Prepare to Evaluate

∴

c ma = (\frac{1}{5.08}) \cdot \int ({3.8}^{2}, x, - \frac{50}{2}, \frac{50}{2})

Next Step Evaluate

∴

c ma = 142.125984251969m

LAST Step Rounding Answer

∴

c ma = 142.126m

Mean Aerodynamic Chord for Propeller-Driven Airplane Formula Elements

Variables

Functions

Mean Aerodynamic Chord

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

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

Chord Length

Chord Length is the length of the airfoil from its leading edge to its trailing edge, parallel to the direction of airflow. It is typically measured in units such as inches, millimeters, or meters.

Symbol: L_c

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Chord Length

Wingspan

The Wingspan (or just span) of a bird or an airplane is the distance from one wingtip to the other wingtip.

Symbol: b

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Wingspan

int

The definite integral can be used to calculate net signed area, which is the area above the x -axis minus the area below the x -axis.

Syntax: int(expr, arg, from, to)

Other formulas in Aircraft Dynamics Nomenclature category

Go Aerodynamic Axial Force

X = C x \cdot q \cdot S

Go Aerodynamic Side Force

Y = C y \cdot q \cdot S

Go Aerodynamic Normal Force

Z = C z \cdot q \cdot S

Go Side force coefficient

C y = \frac{Y}{q \cdot S}

How to Evaluate Mean Aerodynamic Chord for Propeller-Driven Airplane?

Mean Aerodynamic Chord for Propeller-Driven Airplane evaluator uses Mean Aerodynamic Chord = (1/Reference Area)*int(Chord Length^2,x,-Wingspan/2,Wingspan/2) to evaluate the Mean Aerodynamic Chord, Mean Aerodynamic Chord for Propeller-Driven Airplane is a mathematical representation that determines the average aerodynamic chord of a propeller-driven airplane, which is a crucial parameter in assessing its aerodynamic performance, by integrating the squared chord length over the entire wing span. Mean Aerodynamic Chord is denoted by c_ma symbol.

How to evaluate Mean Aerodynamic Chord for Propeller-Driven Airplane using this online evaluator? To use this online evaluator for Mean Aerodynamic Chord for Propeller-Driven Airplane, enter Reference Area (S), Chord Length (L_c) & Wingspan (b) and hit the calculate button.

FAQs on Mean Aerodynamic Chord for Propeller-Driven Airplane

What is the formula to find Mean Aerodynamic Chord for Propeller-Driven Airplane?

The formula of Mean Aerodynamic Chord for Propeller-Driven Airplane is expressed as Mean Aerodynamic Chord = (1/Reference Area)*int(Chord Length^2,x,-Wingspan/2,Wingspan/2). Here is an example- 142.126 = (1/5.08)*int(3.8^2,x,-50/2,50/2).

How to calculate Mean Aerodynamic Chord for Propeller-Driven Airplane?

With Reference Area (S), Chord Length (L_c) & Wingspan (b) we can find Mean Aerodynamic Chord for Propeller-Driven Airplane using the formula - Mean Aerodynamic Chord = (1/Reference Area)*int(Chord Length^2,x,-Wingspan/2,Wingspan/2). This formula also uses Definite Integral (int) function(s).

Can the Mean Aerodynamic Chord for Propeller-Driven Airplane be negative?

No, the Mean Aerodynamic Chord for Propeller-Driven Airplane, measured in Length cannot be negative.

Which unit is used to measure Mean Aerodynamic Chord for Propeller-Driven Airplane?

Mean Aerodynamic Chord for Propeller-Driven Airplane is usually measured using the Meter[m] for Length. Millimeter[m], Kilometer[m], Decimeter[m] are the few other units in which Mean Aerodynamic Chord for Propeller-Driven Airplane can be measured.

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Mean Aerodynamic Chord for Propeller-Driven Airplane Formula

Mean Aerodynamic Chord for Propeller-Driven Airplane Example

Mean Aerodynamic Chord for Propeller-Driven Airplane Solution

Mean Aerodynamic Chord for Propeller-Driven Airplane Formula Elements

Other formulas in Aircraft Dynamics Nomenclature category

How to Evaluate Mean Aerodynamic Chord for Propeller-Driven Airplane?

FAQs on Mean Aerodynamic Chord for Propeller-Driven Airplane

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