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Coefficient of Lift Equation with Coefficient of Normal Force Formula

GoCoefficient of Lift Equation with Angle of Attack Formula

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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. Check FAQs

C L = μ \cdot \cos (α)

C_L - Lift Coefficient?μ - Coefficient of Force?α - Angle of Attack?

Coefficient of Lift Equation with Coefficient of Normal Force Example

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Here is how the Coefficient of Lift Equation with Coefficient of Normal Force equation looks like with Values.

Here is how the Coefficient of Lift Equation with Coefficient of Normal Force equation looks like with Units.

Here is how the Coefficient of Lift Equation with Coefficient of Normal Force equation looks like.

0.4418 = 0.45 \cdot \cos (10.94)

0.4418 = 0.45 \cdot \cos (10.94°)

0.4418 = 0.45 \cdot \cos (10.94)

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Coefficient of Lift Equation with Coefficient of Normal Force Solution

Follow our step by step solution on how to calculate Coefficient of Lift Equation with Coefficient of Normal Force?

FIRST Step Consider the formula

C L = μ \cdot \cos (α)

Next Step Substitute values of Variables

∴

C L = 0.45 \cdot \cos (10.94°)

Next Step Convert Units

∴

C L = 0.45 \cdot \cos (0.1909rad)

Next Step Prepare to Evaluate

∴

C L = 0.45 \cdot \cos (0.1909)

Next Step Evaluate

∴

C L = 0.441821906948958

LAST Step Rounding Answer

∴

C L = 0.4418

Coefficient of Lift Equation with Coefficient of Normal Force Formula Elements

Variables

Functions

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 can be positive or negative.

Formulas to find Lift Coefficient

Coefficient of Force

Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow.

Symbol: μ

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Coefficient of Force

Angle of Attack

Angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.

Symbol: α

Measurement: AngleUnit: °

Note: Value can be positive or negative.

Formulas to find Angle of Attack

cos

Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle.

Syntax: cos(Angle)

Other Formulas to find Lift Coefficient

Go Coefficient of Lift Equation with Angle of Attack

C L = 2 \cdot {(\sin (α))}^{2} \cdot \cos (α)

Other formulas in Newtonian Flow category

Go Exact Normal Shock Wave Maximum Coefficient of Pressure

C p,max = \frac{2}{Y \cdot M^{2}} \cdot (\frac{P T}{P} - 1)

Go Pressure Coefficient for Slender 2D Bodies

C p = 2 \cdot ({(θ)}^{2} + k curvature \cdot y)

Go Pressure Coefficient for Slender Bodies of Revolution

C p = 2 \cdot {(θ)}^{2} + k curvature \cdot y

Go Modified Newtonian Law

C p = C p,max \cdot {(\sin (θ))}^{2}

How to Evaluate Coefficient of Lift Equation with Coefficient of Normal Force?

Coefficient of Lift Equation with Coefficient of Normal Force evaluator uses Lift Coefficient = Coefficient of Force*cos(Angle of Attack) to evaluate the Lift Coefficient, The Coefficient of lift equation with coefficient of normal force formula is defined as product of coefficient of normal force acting on the body and cosine angle of attack. Lift Coefficient is denoted by C_L symbol.

How to evaluate Coefficient of Lift Equation with Coefficient of Normal Force using this online evaluator? To use this online evaluator for Coefficient of Lift Equation with Coefficient of Normal Force, enter Coefficient of Force (μ) & Angle of Attack (α) and hit the calculate button.

FAQs on Coefficient of Lift Equation with Coefficient of Normal Force

What is the formula to find Coefficient of Lift Equation with Coefficient of Normal Force?

The formula of Coefficient of Lift Equation with Coefficient of Normal Force is expressed as Lift Coefficient = Coefficient of Force*cos(Angle of Attack). Here is an example- 0.441822 = 0.45*cos(0.190939020168144).

How to calculate Coefficient of Lift Equation with Coefficient of Normal Force?

With Coefficient of Force (μ) & Angle of Attack (α) we can find Coefficient of Lift Equation with Coefficient of Normal Force using the formula - Lift Coefficient = Coefficient of Force*cos(Angle of Attack). This formula also uses Cosine (cos) function(s).

What are the other ways to Calculate Lift Coefficient?

Here are the different ways to Calculate Lift Coefficient-

Lift Coefficient=2*(sin(Angle of Attack))^2*cos(Angle of Attack)

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