Coefficient of Drag Equation with Angle of Attack Solution

STEP 0: Pre-Calculation Summary
Formula Used
Drag Coefficient = 2*(sin(Angle of Attack))^3
CD = 2*(sin(α))^3
This formula uses 1 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)
Variables Used
Drag Coefficient - The Drag Coefficient is a dimensionless number that quantifies the drag or resistance of an object in a fluid environment, influencing its motion through the fluid.
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
CD = 2*(sin(α))^3 --> 2*(sin(0.1745329251994))^3
Evaluating ... ...
CD = 0.0104722665003896
STEP 3: Convert Result to Output's Unit
0.0104722665003896 --> No Conversion Required
FINAL ANSWER
0.0104722665003896 0.010472 <-- Drag Coefficient
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Verifier Image
Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
Sai Venkata Phanindra Chary Arendra has verified this Calculator and 300+ more calculators!

Newtonian Flow Calculators

Exact Normal Shock Wave Maximum Coefficient of Pressure
​ LaTeX ​ Go Maximum Pressure Coefficient = 2/(Specific Heat Ratio*Mach Number^2)*(Total Pressure/Pressure-1)
Pressure Coefficient for Slender Bodies of Revolution
​ LaTeX ​ Go Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis
Pressure Coefficient for Slender 2D Bodies
​ LaTeX ​ Go Pressure Coefficient = 2*(Angle of Inclination^2+Curvature of Surface*Distance of Point from Centroidal Axis)
Modified Newtonian Law
​ LaTeX ​ Go Pressure Coefficient = Maximum Pressure Coefficient*(sin(Angle of Inclination))^2

Coefficient of Drag Equation with Angle of Attack Formula

​LaTeX ​Go
Drag Coefficient = 2*(sin(Angle of Attack))^3
CD = 2*(sin(α))^3

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 Drag Equation with Angle of Attack?

Coefficient of Drag Equation with Angle of Attack calculator uses Drag Coefficient = 2*(sin(Angle of Attack))^3 to calculate the Drag Coefficient, Coefficient of Drag Equation with Angle of Attack formula is defined as a relationship that quantifies the drag force experienced by an object in a fluid flow, taking into account the angle of attack, which influences aerodynamic performance. Drag Coefficient is denoted by CD symbol.

How to calculate Coefficient of Drag Equation with Angle of Attack using this online calculator? To use this online calculator for Coefficient of Drag Equation with Angle of Attack, enter Angle of Attack (α) and hit the calculate button. Here is how the Coefficient of Drag Equation with Angle of Attack calculation can be explained with given input values -> 0.010472 = 2*(sin(0.1745329251994))^3.

FAQ

What is Coefficient of Drag Equation with Angle of Attack?
Coefficient of Drag Equation with Angle of Attack formula is defined as a relationship that quantifies the drag force experienced by an object in a fluid flow, taking into account the angle of attack, which influences aerodynamic performance and is represented as CD = 2*(sin(α))^3 or Drag Coefficient = 2*(sin(Angle of Attack))^3. 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 Drag Equation with Angle of Attack?
Coefficient of Drag Equation with Angle of Attack formula is defined as a relationship that quantifies the drag force experienced by an object in a fluid flow, taking into account the angle of attack, which influences aerodynamic performance is calculated using Drag Coefficient = 2*(sin(Angle of Attack))^3. To calculate Coefficient of Drag 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 Drag Coefficient?
In this formula, Drag Coefficient uses Angle of Attack. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Drag Coefficient = Coefficient of Force*sin(Angle of Attack)
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!