drgondog
Major
quite well
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He is probably our resident Mustang expert. His father flew it in WW2, and Bill even has some flight time in the P-51D as well.
The three innovative applications of science to airframe for the Mustang was 1.) laminar flow wing/mfg methods to coat and fill rivet sinks, b.) meridith effect to reduce drag (or achieve net thrust depending on which version you want, 3.) second order curve layout of cowl contours to achieve as close to minimum drag.
The Mustang features from day one - lowest drag in the industry until the P-80 and Me 262, longest range from day one (factor of wing fuel and drag) with exception of A6M which sacrificed too much in airframe size to grow with increased tactical mission
Those are my answers and I will stick to them. If I had to guess what Willy had it would be knowledge of Meridith effect as that was in the literature as a theory as early as 1935
The three innovative applications of science to airframe for the Mustang was 1.) laminar flow wing/mfg methods to coat and fill rivet sinks, b.) meridith effect to reduce drag (or achieve net thrust depending on which version you want, 3.) second order curve layout of cowl contours to achieve as close to minimum drag.
Can you elaborate on the use of flush riveting on the Mustang? Specifically this coating/filing of rivet sinks.
I was under the impression that that previous generation of US pursuit aircraft used flush skinning with sunken rivet heads.
Getting away from the cryptic guessing games.
Can you elaborate on the use of flush riveting on the Mustang? Specifically this coating/filing of rivet sinks.
I was under the impression that that previous generation of US pursuit aircraft used flush skinning with sunken rivet heads.
The Japanese started using flush skinning on the Zero in 1940. I recently read an RAAF engineering assessment of the aircraft - a model 32 - and one off the points they were most impressed with compared to their Mk V spitfires was the flush riveting and smoothness of the aircraft skinning.
I came up with either bullet proof windshield or self sealing fuel tanks. Although self sealing tanks seem to be a WWII development, it seems more important than bullet proof windshield. So, I'll say self sealing fuel tanks.
Back to the OP:
P-39 with DB-601/605 and some 30mm firing through prop hub (MK 108 for a dedicated fighter, MK 101/103 for an all-rounder). German 13mm replacing US MGs.
Or, perhaps 3-5 x MG-151/20 (providing 3 can fit between between cockpit and prop reduction gear)
The ejector seat suggestion had nothing to do with your quiz.
Its something that the german aerospace industry had that allies could have done with. Besides the 109 didn't have such seats, Heinkel certainly did on at least three aircraft the 280, 219 and 162, plus sweden first issued a patent for one in 1941 but not Messerschmitt.
By the time Germans were mass producing 30mm cannons, US M4 37mm was reliable
Nevertheless, 'regular' 20-30mm stuff was better bet.