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(i have made this thread as i previously had it in the aero section and it was probably not getting the attention such an important question deserves.)
lets use the sunroof as an example for simplicity.
what force is the wind acting on the dog at 50mph/22.3m/s?
dog head diameter = 0.2m
therefore frontal area of dog head is 0.0314m^2
Drag coefficient = 2
air density = 1.22
here is my attempt (#1) based on wall loading calculations:
0.00256 * 50 * 50 = 6.4 lb/ sq feet = 306.4Pa
0.0314 * 306.4 * 2=19.25N
here is my attempt (2) based on drag equation
2 x ((1.22 x 50^2)/2) * 0.0314 = 19N
any thoughts
lets use the sunroof as an example for simplicity.
what force is the wind acting on the dog at 50mph/22.3m/s?
dog head diameter = 0.2m
therefore frontal area of dog head is 0.0314m^2
Drag coefficient = 2
air density = 1.22
here is my attempt (#1) based on wall loading calculations:
0.00256 * 50 * 50 = 6.4 lb/ sq feet = 306.4Pa
0.0314 * 306.4 * 2=19.25N
here is my attempt (2) based on drag equation
2 x ((1.22 x 50^2)/2) * 0.0314 = 19N
any thoughts