Quote:
Originally Posted by slipknotsv
Mr. aerohead please comment 
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Scientifically,and from empirical research in wind tunnels,the lowest drag nose,for sub-sonic,incompressible flow,is half of a convex hemisphere,or,'bulbous' nose.
It allows for essentially-ideal,symmetrical, uniform streamline acceleration,directing,over and around the body.with a minimum of surface area (friction),and absence of pressure spikes,with full attachment,and enough camber to set up divergent aft-body flow.
Here it is in 2-D flow
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Notice the effect of the aft-body.
Once it reaches supercritical Reynolds number (20-mph with a car),there's full attachment right into the aft-body.(3-D flow)
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Here it is underwater
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It's perfect!
Here's the origin of the perfect subsonic shape,dating to as early as 1898,with Gustav Eiffel and his famous vertical wind tunnel,Eiffel Tower in Paris.(think ice cream cone)
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