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Need help understanding drag forces in external flow past immersed bodies (Flat plates, airfoils, ect)
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Hey everyone. I'm having trouble understanding where and what area is affected by drag when flow is moving past a immersed body, like a flat plate for example.

In my textbook : Fluid Mechanics by Frank M. White, the Coefficient of Drag, is: C_d = (2Drag)/(DensityVelocity_squared*Area).

From my understanding the Area portion of the formula is either the frontal area, or the planform area (area from the top view). A few the problems in the text use the length and height of the shape, not the length and width (into the page). Can anyone explain why?

This is the question I was referring to : http://www.sfu.ca/~ptaherib/teaching/ENSC_283_2013/Suggested Problems/Suggested Problems Chapter 7/P7.56.pdf

Thanks in advance!

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10 years ago