Calculating Drag Coefficient for Skydiving Research

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SUMMARY

This discussion focuses on calculating the drag coefficient (Cd) for skydiving research using the drag equation D = Cd ((rV^2)/2)A. The air density (r) is specified as 1.2 kg/m^3, and the approximate area (A) of the skydiver is measured at 0.871 square meters. The drag coefficient is not a constant but varies based on the object's shape and the fluid's properties, such as air. Experimental measurement is the primary method for determining Cd, as it cannot be easily calculated.

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  • Understanding of fluid dynamics principles
  • Familiarity with the drag equation
  • Knowledge of Reynolds number and its significance
  • Basic experimental measurement techniques
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  • Explore the relationship between shape and drag coefficient in various fluids
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Aerodynamics researchers, skydiving instructors, and anyone involved in performance optimization for skydiving or similar activities.

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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