Re: Aerodynamic modifications
Fire away. Fun commenting on details like this. Desirable pressure recovery on the ass end should be the goal. Reducing airframe volume decreases drag too, but if the close outs are too severe, the displacement thickness, or boundary layer growth, effectively increases airframe volume too. You just can't see it. Can you post pictures of the Furias and 232 decks. Remember, 232 has a longer fuselage than the 'Stangs, so dimensionally, 232's deck might be the same, or similar to Dago's in length.
Originally posted by CJAM427
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