P-47 size comparison.

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Jimmy Doolittle received a doctorate in aeronautics from MIT in 1925, the first issued in the United States. (source: Wiki) Aeronautics was, at the time, an "emerging technology."

In my time there, I heard that Doolittle hung a plane upside down at MIT and very carefully piled sandbags on the wings until they cracked. That allowed him to determine the structural G-limit. However, that work may have been mis-attributed--still done at MIT, but by someone else.
 
First, the important question: how big would the P-47 have to be to carry eight 20mm ShVak? Otherwise, you might as well compare the Spitfire to the La-5 and ask what the La-5 would need to do to carry 8 guns.

The ShVak was a high-performance cannon, and much larger and heavier than the M2, so the La-5 didn't need as many guns as the 8x .50 hung on a Thunderbolt.

(I understand your general point, which is completely accurate, but there's also "Horses for courses." If you're not trying to fight in the stratosphere, or something equally ridiculous, there's no reason to drag around all sorts of equipment to boost your performance at altitude.)
 
P-47 had a lot o' junk in the trunk


View attachment 701182
Thank you. the duct work and then the fuel tanks explain the thickness of the fuselage. I am wondering if the Hellcat fuselage plus the ductwork would equal the seat height (from the bottom exterior of the fuselage) between the Hellcat and the Thunderbolt. I love all the cutaways and drawings showing where things were.
 
The ShVak was a high-performance cannon, and much larger and heavier than the M2, so the La-5 didn't need as many guns as the 8x .50 hung on a Thunderbolt.
ShVak weighed 42kg.
M2 weighed 29KG,
P-47 was carrying 2.8 times the weight of guns, closer to 4 times the amount of ammo?
The M2 was not very weight efficient but the airplane makes doesn't pick the guns, The government does and the airplane maker tries to fit them in.
Anybody want to compare the Mig-3 size AND Weight to the P-47 as the Soviet plane that came closest to the speed/altitude of P-47 and check the weight of the armament?
 
Wandering off-topic, I just got off the phone with my father. I was telling him about my visit to Le Bourget and contrasting the construction of the Yak-9 with American production in WWII especially the use of a single hydraulic press to stamp and cut pieces in the same operation.

My father identified this as the Guerin process, which popped the name back into my memory. It turns out the Henry Guerin was his first boss in California. Guerin showed him how the process worked and showed him the resistance welding techniques they were using. The company was combining these techniques in hope of producing the first stainless steel honeycombs. Guerin then set my father loose to machine the dies and weld the first samples (some of them are in the shed in his back yard). My father was 18 and was given pretty general instructions and light supervision.

Anyhow, the Guerin process was developed at Douglas Aircraft. Henry Guerin was the managing director of Douglas' Santa Monica plant in WWII and had personally developed the method.

It's not clear to me whether or not Guerin had a college degree. I don't know (yet) how much Guerin influenced my father, but my father never got a degree, but he did take engineering classes at UCLA. That did not stop him from having a career as an engineer, either. I wouldn't say that my father puled it off because he was smarter than other engineers, but my father does combine a lot of common sense, practicality, and ability to see to the heart of matters, and is driven nuts by inefficiency and poor design.

I may move some of this to a separate topic after I get further information. It probably belongs in "Not WWII."
 
Excellent graphic!
 
I know the historical records proves otherwise, but to me this never looked like something that should be introduced into a shooting environment.
Most everything aft of the engine except the turbo itself (all the way to right) was an air duct of some some sort.
It could affect the performance of the system (power at altitude) but would not stop it. Plane could continue flying for hours with dozen of holes in the tubes/ducts.
Not like holes in the radiator or oil cooler.
It may need an awful lot of repair work once it got home
 

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