Coefficient of Drag Equation with Coefficient of Normal Force Calculator

✖The Coefficient of Force is a dimensionless value that characterizes the relationship between force and flow in Newtonian fluids under hypersonic conditions.ⓘ Coefficient of Force [μ]			+10% -10%
✖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]			+10% -10%

✖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.ⓘ Coefficient of Drag Equation with Coefficient of Normal Force [C_D]

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Coefficient of Drag Equation with Coefficient of Normal Force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Drag Coefficient = Coefficient of Force*sin(Angle of Attack)
C_D = μ*sin(α)
This formula uses 1 Functions, 3 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.
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.
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

Coefficient of Force: 0.06 --> No Conversion Required
Angle of Attack: 10 Degree --> 0.1745329251994 Radian (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_D = μ*sin(α) --> 0.06*sin(0.1745329251994)

Evaluating ... ...

C_D = 0.0104188906600139

STEP 3: Convert Result to Output's Unit

0.0104188906600139 --> No Conversion Required

FINAL ANSWER

0.0104188906600139 ≈ 0.010419 <-- Drag 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 Drag Equation with Coefficient of Normal Force Formula

Drag Coefficient = Coefficient of Force*sin(Angle of Attack)
C_D = μ*sin(α)

What is angle of attack?

n fluid dynamics, angle of attack is the angle between a reference line on a body (often the chord line of an airfoil) 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 Coefficient of Normal Force?

Coefficient of Drag Equation with Coefficient of Normal Force calculator uses Drag Coefficient = Coefficient of Force*sin(Angle of Attack) to calculate the Drag Coefficient, Coefficient of Drag Equation with Coefficient of Normal Force formula is defined as a relationship that describes the drag force experienced by an object moving through a fluid, influenced by the object's normal force and the angle of attack. Drag Coefficient is denoted by C_D symbol.

How to calculate Coefficient of Drag Equation with Coefficient of Normal Force using this online calculator? To use this online calculator for Coefficient of Drag Equation with Coefficient of Normal Force, enter Coefficient of Force (μ) & Angle of Attack (α) and hit the calculate button. Here is how the Coefficient of Drag Equation with Coefficient of Normal Force calculation can be explained with given input values -> 0.078142 = 0.06*sin(0.1745329251994).

FAQ

What is Coefficient of Drag Equation with Coefficient of Normal Force?

Coefficient of Drag Equation with Coefficient of Normal Force formula is defined as a relationship that describes the drag force experienced by an object moving through a fluid, influenced by the object's normal force and the angle of attack and is represented as C_D = μ*sin(α) or Drag Coefficient = Coefficient of Force*sin(Angle of Attack). The Coefficient of Force is a dimensionless value that characterizes the relationship between force and flow in Newtonian fluids under hypersonic conditions & 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 Coefficient of Normal Force?

Coefficient of Drag Equation with Coefficient of Normal Force formula is defined as a relationship that describes the drag force experienced by an object moving through a fluid, influenced by the object's normal force and the angle of attack is calculated using Drag Coefficient = Coefficient of Force*sin(Angle of Attack). To calculate Coefficient of Drag Equation with Coefficient of Normal Force, you need Coefficient of Force (μ) & Angle of Attack (α). With our tool, you need to enter the respective value for Coefficient of Force & 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 Coefficient of Force & Angle of Attack. We can use 1 other way(s) to calculate the same, which is/are as follows -

Drag Coefficient = 2*(sin(Angle of Attack))^3

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