Aeroweanie's latest activity
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Aeroweanie commented on Shortways's profile post.This page from a Bf 109F document says it stayed at 1.7 deg: -
Aeroweanie replied to the thread Wing profile of Ho 229.By "elevator" I mean the pitch axis control surface.
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Aeroweanie replied to the thread Wing profile of Ho 229.Pitch stability is dependent on the rate of change of pitching moment with lift, not the actual value of the pitching moment. The...
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Aeroweanie replied to the thread Wing profile of Ho 229.Pitch stability is dependent on the rate of change of pitching moment with lift, not the actual value of the pitching moment. The...
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Aeroweanie replied to the thread Wing profile of Ho 229.I figured it out from this drawing. The airfoil is a AVA 0 0 12.598-2 28/.55 thickness form added to camber from a NACA 1.1151R2 12.598...
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Aeroweanie replied to the thread Interpreting certain German airfoils.Very overdue, but the answer is: this provides a means of creating NACA modified 4-digit airfoils using a method developed by the AVA...
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Aeroweanie replied to the thread P51D Wing & Fuselage Ordinates.Its a lot of typing, but these are the loft coordinates of the P-51D/K wing. Be careful, as the wing of the P-51B/C and P-51H are...
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Aeroweanie replied to the thread Non-WWII Aircraft drawings?.This website is worth knowing about, but they don't seem to have the Potez IX: RCL : 3views
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Aeroweanie replied to the thread Original blueprints (physical).These days, the distinctions have become blurred, as while I have paper drawings of aircraft like the Spitfire, they are reproductions...
