Coefficient of Lift Equation with Angle of Attack Calculator

✖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.ⓘ Angle of Attack [α]

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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.ⓘ Coefficient of Lift Equation with Angle of Attack [C_L]

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Coefficient of Lift Equation with Angle of Attack Solution

STEP 0: Pre-Calculation Summary

Formula Used

Lift Coefficient = 2*(sin(Angle of Attack))^2*cos(Angle of Attack)
C_L = 2*(sin(α))^2*cos(α)
This formula uses 2 Functions, 2 Variables

Functions Used

sin - Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse., sin(Angle)
cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)

Variables Used

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.
Angle of Attack - (Measured in Radian) - 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.

STEP 1: Convert Input(s) to Base Unit

Angle of Attack: 10 Degree --> 0.1745329251994 Radian (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_L = 2*(sin(α))^2*cos(α) --> 2*(sin(0.1745329251994))^2*cos(0.1745329251994)

Evaluating ... ...

C_L = 0.0593911746138628

STEP 3: Convert Result to Output's Unit

0.0593911746138628 --> No Conversion Required

FINAL ANSWER

0.0593911746138628 ≈ 0.059391 <-- Lift Coefficient

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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Coefficient of Lift Equation with Angle of Attack Formula

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

What is angle of attack?

In fluid dynamics, 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.

How to Calculate Coefficient of Lift Equation with Angle of Attack?

Coefficient of Lift Equation with Angle of Attack calculator uses Lift Coefficient = 2*(sin(Angle of Attack))^2*cos(Angle of Attack) to calculate the Lift Coefficient, Coefficient of Lift Equation with Angle of Attack formula is defined as a relationship that quantifies the lift generated by an airfoil based on the angle of attack, influencing aerodynamic performance in fluid mechanics. Lift Coefficient is denoted by C_L symbol.

How to calculate Coefficient of Lift Equation with Angle of Attack using this online calculator? To use this online calculator for Coefficient of Lift Equation with Angle of Attack, enter Angle of Attack (α) and hit the calculate button. Here is how the Coefficient of Lift Equation with Angle of Attack calculation can be explained with given input values -> 0.059391 = 2*(sin(0.1745329251994))^2*cos(0.1745329251994).

FAQ

What is Coefficient of Lift Equation with Angle of Attack?

Coefficient of Lift Equation with Angle of Attack formula is defined as a relationship that quantifies the lift generated by an airfoil based on the angle of attack, influencing aerodynamic performance in fluid mechanics and is represented as C_L = 2*(sin(α))^2*cos(α) or Lift Coefficient = 2*(sin(Angle of Attack))^2*cos(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.

How to calculate Coefficient of Lift Equation with Angle of Attack?

Coefficient of Lift Equation with Angle of Attack formula is defined as a relationship that quantifies the lift generated by an airfoil based on the angle of attack, influencing aerodynamic performance in fluid mechanics is calculated using Lift Coefficient = 2*(sin(Angle of Attack))^2*cos(Angle of Attack). To calculate Coefficient of Lift Equation with Angle of Attack, you need Angle of Attack (α). With our tool, you need to enter the respective value for Angle of Attack and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Lift Coefficient?

In this formula, Lift Coefficient uses Angle of Attack. We can use 1 other way(s) to calculate the same, which is/are as follows -

Lift Coefficient = Coefficient of Force*cos(Angle of Attack)

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