Aerodynamic Axial Force Calculator

✖Axial Force Coefficient is the dimensionless coefficient associated with the component of aerodynamic forces along the roll axis on an aircraft.ⓘ Axial Force Coefficient [C_x]			+10% -10%
✖Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.ⓘ Dynamic Pressure [q]			+10% -10%
✖The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.ⓘ Reference Area [S]			+10% -10%

✖Aerodynamic Axial Force is the component of aerodynamic force along the roll axis of an aircraft.ⓘ Aerodynamic Axial Force [X]

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Aerodynamic Axial Force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Aerodynamic Axial Force = Axial Force Coefficient*Dynamic Pressure*Reference Area
X = C_x*q*S
This formula uses 4 Variables

Variables Used

Aerodynamic Axial Force - (Measured in Newton) - Aerodynamic Axial Force is the component of aerodynamic force along the roll axis of an aircraft.
Axial Force Coefficient - Axial Force Coefficient is the dimensionless coefficient associated with the component of aerodynamic forces along the roll axis on an aircraft.
Dynamic Pressure - (Measured in Pascal) - Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Reference Area - (Measured in Square Meter) - The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.

STEP 1: Convert Input(s) to Base Unit

Axial Force Coefficient: 0.67 --> No Conversion Required
Dynamic Pressure: 10 Pascal --> 10 Pascal No Conversion Required
Reference Area: 5.08 Square Meter --> 5.08 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

X = C_x*q*S --> 0.67*10*5.08

Evaluating ... ...

X = 34.036

STEP 3: Convert Result to Output's Unit

34.036 Newton --> No Conversion Required

FINAL ANSWER

34.036 Newton <-- Aerodynamic Axial Force

(Calculation completed in 00.004 seconds)

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Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

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Verified by Shikha Maurya

Indian Institute of Technology (IIT), Bombay

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< Aircraft Dynamics Nomenclature Calculators

Aerodynamic Normal Force

LaTeX Go Aerodynamic Normal Force = Normal Force Coefficient*Dynamic Pressure*Reference Area

Aerodynamic Axial Force

LaTeX Go Aerodynamic Axial Force = Axial Force Coefficient*Dynamic Pressure*Reference Area

Side force coefficient

LaTeX Go Side Force Coefficient = Aerodynamic Side Force/(Dynamic Pressure*Reference Area)

Aerodynamic Side Force

LaTeX Go Aerodynamic Side Force = Side Force Coefficient*Dynamic Pressure*Reference Area

Aerodynamic Axial Force Formula

LaTeX Go

Aerodynamic Axial Force = Axial Force Coefficient*Dynamic Pressure*Reference Area
X = C_x*q*S

What are the two aerodynamic forces?

By convention, the single aerodynamic force is broken into two components: the drag force, which is opposed to the direction of motion, and the lift force, which acts perpendicular to the motion.

How to Calculate Aerodynamic Axial Force?

Aerodynamic Axial Force calculator uses Aerodynamic Axial Force = Axial Force Coefficient*Dynamic Pressure*Reference Area to calculate the Aerodynamic Axial Force, Aerodynamic Axial Force is a measure of the force exerted in the direction of motion, determined by the axial force coefficient, dynamic pressure, and reference area, providing a crucial parameter in aerodynamic analysis. Aerodynamic Axial Force is denoted by X symbol.

How to calculate Aerodynamic Axial Force using this online calculator? To use this online calculator for Aerodynamic Axial Force, enter Axial Force Coefficient (C_x), Dynamic Pressure (q) & Reference Area (S) and hit the calculate button. Here is how the Aerodynamic Axial Force calculation can be explained with given input values -> 34.036 = 0.67*10*5.08.

FAQ

What is Aerodynamic Axial Force?

Aerodynamic Axial Force is a measure of the force exerted in the direction of motion, determined by the axial force coefficient, dynamic pressure, and reference area, providing a crucial parameter in aerodynamic analysis and is represented as X = C_x*q*S or Aerodynamic Axial Force = Axial Force Coefficient*Dynamic Pressure*Reference Area. Axial Force Coefficient is the dimensionless coefficient associated with the component of aerodynamic forces along the roll axis on an aircraft, Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid & The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.

How to calculate Aerodynamic Axial Force?

Aerodynamic Axial Force is a measure of the force exerted in the direction of motion, determined by the axial force coefficient, dynamic pressure, and reference area, providing a crucial parameter in aerodynamic analysis is calculated using Aerodynamic Axial Force = Axial Force Coefficient*Dynamic Pressure*Reference Area. To calculate Aerodynamic Axial Force, you need Axial Force Coefficient (C_x), Dynamic Pressure (q) & Reference Area (S). With our tool, you need to enter the respective value for Axial Force Coefficient, Dynamic Pressure & Reference Area and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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