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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 number that represents the lift generated by a body in a fluid flow, crucial for understanding aerodynamic performance. 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.

0.0591 = 0.06 \cdot \cos (10)

0.0591 = 0.06 \cdot \cos (10°)

0.0591 = 0.06 \cdot \cos (10)

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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 = 0.06 \cdot \cos (10°)

Next Step Convert Units

∴

C L = 0.06 \cdot \cos (0.1745rad)

Next Step Prepare to Evaluate

∴

C L = 0.06 \cdot \cos (0.1745)

Next Step Evaluate

∴

C L = 0.0590884651807328

LAST Step Rounding Answer

∴

C L = 0.0591

Coefficient of Lift Equation with Coefficient of Normal Force Formula Elements

Variables

Functions

Lift Coefficient

The Lift Coefficient is a dimensionless number that represents the lift generated by a body in a fluid flow, crucial for understanding aerodynamic performance.

Symbol: C_L

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Lift Coefficient

Coefficient of Force

The Coefficient of Force is a dimensionless value that characterizes the relationship between force and flow in Newtonian fluids under hypersonic conditions.

Symbol: μ

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Coefficient of Force

Angle of Attack

The Angle of Attack is the angle between the chord line of an airfoil and the oncoming airflow, influencing lift and drag in fluid dynamics.

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 c \cdot y)

Go Pressure Coefficient for Slender Bodies of Revolution

C p = 2 \cdot {(θ)}^{2} + k c \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, Coefficient of Lift Equation with Coefficient of Normal Force formula is defined as a relationship that describes how the lift generated by an object in a fluid is influenced by the normal force and the angle of attack, impacting aerodynamic performance. 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- 0.059088 = 0.06*cos(0.1745329251994).

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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