Drag & Downforce

Drag

Drag Force predominantly depends upon the velocity, frontal area, and coefficient of drag of the body. It can be expressed as:

Drag Formula

(Fd)=0.5\ Cd ρ A V²

Where Fd is the drag force;
ρ is the density of fluid medium that is air;
A is the frontal area of the body facing the fluid;
V is the velocity of the body;
Cd is the coefficient of drag of the body.

Lift

Lift force can be expressed as:

Lift Formula

Fl=0.5\ Cl ρ A V²

Where FL is the lift force;
ρ is the density of fluid medium that is air;
A is the frontal area of the body facing the fluid;
V is the velocity of the body;
Cl is the coefficient of lift of the body.

Flow Separation

Flow Separation

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Aerodynamic Devices

1. Spoiler

Spoiler

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2. Wing

Wing

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3. Fins

Fins

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4. Diffuser

Diffuser

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Additional Reading Material

Research Paper

This is a research paper on effects of various Aerodynamic Devices & their effects when used in combination to maximize performance output of Racecar

https://aia.springeropen.com/articles/10.1186/s42774-020-00054-7

Scan QR Code or Click to view the Springer Article on Passive Aerodynamic Devices