Quote:
Originally Posted by kach22i
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*The dimensions remain constant
*Only the features of the fuselage vary,from 'bare',to fully festooned with canopy opening with pilot,windscreen,and engine.
*The Cds are a function of Reynolds number (read along the bottom ),as an aircraft fuselage is large enough the be affected by skin friction more so than pressure drag.
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It appears that your fuselage tool is for supersonic aircraft,based on the nose architecture.
We'd want the blunt nose for 'normal' driving velocities.