picklefeet
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I know the equation for terminal velocity and drag coefficient. But I can't find one without the other. It's a real catch-22. I also don't know the Drag Force. HEEELP!
The discussion revolves around the relationship between drag coefficient (Cd) and terminal velocity, particularly in the context of a quarter falling through air. Participants explore the challenges of calculating drag force and terminal velocity without knowing one of the variables, and the implications of Reynolds number on drag coefficient.
Participants express various viewpoints on the relationship between drag coefficient, Reynolds number, and the specific scenario of a falling quarter. There is no consensus on the best approach to calculate the drag coefficient or terminal velocity, and multiple competing views remain regarding the significance of Reynolds number in this context.
Some limitations include the dependence on assumptions about the stability of the quarter's orientation and the potential variability of drag coefficient with changing conditions. The discussion also reflects uncertainty about the appropriate conditions for applying different drag force models.
This is getting past what Aero I took, but isn't that only for situations where viscous drag changes a lot? Can't we just use this equation there: http://www.grc.nasa.gov/WWW/K-12/airplane/drageq.htmlFredGarvin said:Cd is a function of Reynolds Number.