Along with every real-world diagram I've ever seen.I was looking for reference diagrams, the ones I was finding for actual aircraft tended to have the CoG range entirely ahead of the Co
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Along with every real-world diagram I've ever seen.I was looking for reference diagrams, the ones I was finding for actual aircraft tended to have the CoG range entirely ahead of the Co
Along with every real-world diagram I've ever seen.
Hello Ivan,I am wondering now what a diagram for the rather common Cessna 172 looks like. I had found a diagram of a Cessna earlier but with the CoG limits ahead of CoL. I did not save it, so I don't know what model Cessna it was and if they differ that much between models.
However, I think the decision to put the engine behind the pilot was based on an attempt to have the center of gravity and the most mass in a central location.
While that may be part of it, it really was all about the big cannon.
That big, heavy, almost useless in air-to-air combat 37mm cannon.
The USAAC/F loved it. It was supposed to be in the P-38. Two were in the XP-54 (needed a special tilting nose to be able to shoot the 37mm guns at the same target as the 0.50" mgs) and the XP-67 was to have 6 (! ) of the 37mm cannon.
Anyway, the only practical way to have a gun firing through the hub of an aircraft equipped with a V-1710 was with a remote drive. Such a remote drive featured in other proposed layouts by Bell and Curtiss, usually with smaller cannon (20-25mm) and with front engines. The 37mm needed more space, however.
The author also states that it was planned that the 37 mm cannon could be replaced by 20 mm depending on the need.
Was this ever done?
The P-400 (a P-39 built for the Brits but they didn't want) had the 20mm HS cannon. According to Wagner, these were called the Model 14 my Bell and the P-400 by USAAF. Wagner reports 675 were built and the U.S. ended up with 179. The P-400s were used a lot on Guadalcanal.The author also states that it was planned that the 37 mm cannon could be replaced by 20 mm depending on the need.
Was this ever done?
While that may be part of it, it really was all about the big cannon.
That big, heavy, almost useless in air-to-air combat 37mm cannon.
The USAAC/F loved it. It was supposed to be in the P-38. Two were in the XP-54 (needed a special tilting nose to be able to shoot the 37mm guns at the same target as the 0.50" mgs) and the XP-67 was to have 6 (! ) of the 37mm cannon.
Anyway, the only practical way to have a gun firing through the hub of an aircraft equipped with a V-1710 was with a remote drive. Such a remote drive featured in other proposed layouts by Bell and Curtiss, usually with smaller cannon (20-25mm) and with front engines. The 37mm needed more space, however.
The XP-40 did have a belly-radiator, it didn't work so they moves it up to the nose...Not only that but in putting an in line engine in, the radiator was mounted there with it, which is not the best place, compared to the P51 and others which was designed from the start with an inline engine with radiators mounted elsewhere.
Wait... I didn't think the A-320 was designed to be unstable, merely used FBW to reduce weight...Actually some fly-by-wire planes with active stability do derive useful positive lift from the tail, but this only works safely with a computer making constant tiny corrections with the control surfaces. That's why the A320 is more fuel efficient than the very similar 737-800.