Aerodynamic Drag Force Calculator

✖Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.ⓘ Drag Coefficient [C_drag]			+10% -10%
✖Mass Density is a representation of the amount of mass (or the number of particles) of a substance, material or object in relation to the space.ⓘ Mass Density [ρ]			+10% -10%
✖Flow Velocity is the vector field that is used to describe fluid motion in a mathematical manner. The entire length of the flow velocity is referred to as the flow speed.ⓘ Flow Velocity [V_f]			+10% -10%
✖The Reference Area A is typically the cross-sectional or frontal area of the object, but may also be the surface area (wetted area) or other representative area describing the object.ⓘ Reference Area [A_ref]			+10% -10%

✖Drag Force is the aerodynamic force that opposes an aircraft's motion through the air. Drag is generated by every part of the airplane.ⓘ Aerodynamic Drag Force [F_drag]

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Aerodynamic Drag Force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Drag Force = Drag Coefficient*((Mass Density*Flow Velocity^2)/2)*Reference Area
F_drag = C_drag*((ρ*V_f^2)/2)*A_ref
This formula uses 5 Variables

Variables Used

Drag Force - (Measured in Newton) - Drag Force is the aerodynamic force that opposes an aircraft's motion through the air. Drag is generated by every part of the airplane.
Drag Coefficient - Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
Mass Density - (Measured in Kilogram per Cubic Meter) - Mass Density is a representation of the amount of mass (or the number of particles) of a substance, material or object in relation to the space.
Flow Velocity - (Measured in Meter per Second) - Flow Velocity is the vector field that is used to describe fluid motion in a mathematical manner. The entire length of the flow velocity is referred to as the flow speed.
Reference Area - (Measured in Square Meter) - The Reference Area A is typically the cross-sectional or frontal area of the object, but may also be the surface area (wetted area) or other representative area describing the object.

STEP 1: Convert Input(s) to Base Unit

Drag Coefficient: 1.39 --> No Conversion Required
Mass Density: 98 Kilogram per Cubic Meter --> 98 Kilogram per Cubic Meter No Conversion Required
Flow Velocity: 6.4 Kilometer per Hour --> 1.77777777777778 Meter per Second (Check conversion here)
Reference Area: 5.07 Square Meter --> 5.07 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

F_drag = C_drag*((ρ*V_f^2)/2)*A_ref --> 1.39*((98*1.77777777777778^2)/2)*5.07

Evaluating ... ...

F_drag = 1091.37445925926

STEP 3: Convert Result to Output's Unit

1091.37445925926 Newton --> No Conversion Required

FINAL ANSWER

1091.37445925926 ≈ 1091.374 Newton <-- Drag Force

(Calculation completed in 00.004 seconds)

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Credits

Created by Aditya Prakash Gautam

Indian Institute of Technology (IIT (ISM) ), Dhanbad, Jharkhand

Aditya Prakash Gautam has created this Calculator and 25+ more calculators!

Verified by Peri Krishna Karthik

National Institute of Technology Calicut (NIT Calicut), Calicut, Kerala

Peri Krishna Karthik has verified this Calculator and 8 more calculators!

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LaTeX Go Torque = 1.35*((Back Emf*AC Line Voltage*Rectified Rotor Current*RMS Value of Rotor Side Line Voltage)/(Back Emf*Angular Frequency))

Aerodynamic Drag Force

LaTeX Go Drag Force = Drag Coefficient*((Mass Density*Flow Velocity^2)/2)*Reference Area

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Aerodynamic Drag Force Formula

LaTeX Go

Drag Force = Drag Coefficient*((Mass Density*Flow Velocity^2)/2)*Reference Area
F_drag = C_drag*((ρ*V_f^2)/2)*A_ref

What is Aerodynamic Drag ?

Aerodynamic Drag is a force which the oncoming air applies on a moving body. It is the resistance offered by the air to the movement of the body. So, when a car is moving; it displaces the air. However, it affects the car’s speed and performance. Technically, it is the aerodynamic drag or the friction offered by the air to a vehicle.

How to Calculate Aerodynamic Drag Force?

Aerodynamic Drag Force calculator uses Drag Force = Drag Coefficient*((Mass Density*Flow Velocity^2)/2)*Reference Area to calculate the Drag Force, The Aerodynamic Drag Force equation states that drag force is equal to the drag coefficient times the mass density times half of the flow velocity squared times the reference area. Drag Force is denoted by F_drag symbol.

How to calculate Aerodynamic Drag Force using this online calculator? To use this online calculator for Aerodynamic Drag Force, enter Drag Coefficient (C_drag), Mass Density (ρ), Flow Velocity (V_f) & Reference Area (A_ref) and hit the calculate button. Here is how the Aerodynamic Drag Force calculation can be explained with given input values -> 1091.374 = 1.39*((98*1.77777777777778^2)/2)*5.07.

FAQ

What is Aerodynamic Drag Force?

The Aerodynamic Drag Force equation states that drag force is equal to the drag coefficient times the mass density times half of the flow velocity squared times the reference area and is represented as F_drag = C_drag*((ρ*V_f^2)/2)*A_ref or Drag Force = Drag Coefficient*((Mass Density*Flow Velocity^2)/2)*Reference Area. Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water, Mass Density is a representation of the amount of mass (or the number of particles) of a substance, material or object in relation to the space, Flow Velocity is the vector field that is used to describe fluid motion in a mathematical manner. The entire length of the flow velocity is referred to as the flow speed & The Reference Area A is typically the cross-sectional or frontal area of the object, but may also be the surface area (wetted area) or other representative area describing the object.

How to calculate Aerodynamic Drag Force?

The Aerodynamic Drag Force equation states that drag force is equal to the drag coefficient times the mass density times half of the flow velocity squared times the reference area is calculated using Drag Force = Drag Coefficient*((Mass Density*Flow Velocity^2)/2)*Reference Area. To calculate Aerodynamic Drag Force, you need Drag Coefficient (C_drag), Mass Density (ρ), Flow Velocity (V_f) & Reference Area (A_ref). With our tool, you need to enter the respective value for Drag Coefficient, Mass Density, Flow Velocity & 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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