Calculating Drag Coefficient for Skydiving Research

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The discussion focuses on calculating the drag coefficient (Cd) for skydiving research using the drag equation D = Cd ((rV^2)/2)A. The user is utilizing an air density of 1.2 kg/m^3 and an approximate skydiver area of 0.871 square meters. Cd is not a constant but varies based on the object's shape and the fluid it moves through, with its calculation typically requiring experimental measurement rather than a straightforward formula. The influence of Reynolds number on Cd is minimal, and resources for experimental data on Cd for various shapes are suggested. Understanding Cd is crucial for accurately assessing drag in skydiving scenarios.
Hazarrd
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Im doing research on skydiving and I am trying to find out how much drag is created on different jumps. I have different velocities for each of the jumps.

D = Cd ((rV^2)/2)A

That is the equation I am using. r is air density which I am using 1.2 kg/m^3. V is the velocity. And I've measured the skydivers approximate area (A) to be .871 square meters. How do I find Cd (Drag coefficient)? Is this a constant? Is there somewhere I can get some more information on what Cd would be? Thanks!
 
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you have to calculate the coeffiecent on a basis where that is the unknown and then just re arrange, and to my belief the drag co-efficient is a constant that varies with the fluid the object is traveling in be it air water or honey.
 
Cd depends mostly on the shape of the object, and very weakly on something called Reynold's number. There's no simple way to calculate Cd, so its usually just measured experimentally. Here are some examples with simple shapes: http://www.insideracingtechnology.com/tech102drag.htm.
 
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