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Does drag coefficient change with size?

Does drag coefficient change with size?

The drag coefficient will change with size because the Reynolds number will change and the ratio of viscous and inertial forces will be different. One can sometimes alter the fluid conditions so that a scale model will have a Reynolds number near that of the actual body and the drag coefficient will be more meaningful.

What does a drag coefficient of 1 mean?

The Reynolds number will be low for small objects, low velocities, and high viscosity fluids. A equal to 1 would be obtained in a case where all of the fluid approaching the object is brought to rest, building up stagnation pressure over the whole front surface.

Does drag coefficient change with shape?

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A quick comparison shows that a flat plate gives the highest drag and a streamlined symmetric airfoil gives the lowest drag, by a factor of almost 30! Shape has a very large effect on the amount of drag produced.

Do all spheres have the same drag coefficient?

All spheres have the same shape, just different radii. The drag coefficient is a non-dimensional quantity which relates drag force with other key variables, like fluid velocity, density, and some physical characteristic of the body in question.

What is the drag coefficient of a Formula 1 car?

between 0.7 and 1.1
Typical Formula 1 car drag coefficients are between 0.7 and 1.1, depending on the circuit the car is set up for. ! A lot of this drag is due to the wings but a lot of it is due to the uncovered wheels.

Is higher or lower coefficient of drag better?

A low coefficient is conducive to high top speed and low fuel consumption, while a higher drag coefficient is generally found in cars searching for high cornering speeds influenced by downforce. It shows that a car’s coefficient of drag can be found by analysing the drag force acting on the car at a given speed.

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What determines the drag coefficient?

The drag coefficient is a number that aerodynamicists use to model all of the complex dependencies of shape, inclination, and flow conditions on aircraft drag. The drag coefficient Cd is equal to the drag D divided by the quantity: density r times half the velocity V squared times the reference area A.