March until October of 1940: fighters' ranking

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I could be wrong, but I have been under the impression they were designed to allow for clearance for the large prop, and that the reduced drag was an ancillary benefit noticed later. I'm happy to be corrected if I am wrong. Getting good dope is why I read here.
The issues of the landing gear and prop were addressed by the gull wing.
 
In WWII, the Americans had more engineering resources than anyone else. The fact remains that the Mustang was designed mostly in a panic rush by people with limited experience in fighter design. It all worked out in the end, but it was not a good war strategy.

The Germans had their share of good aircraft and engine designers, but they missed the laminar flow wings and two-stage superchargers.
That is your opinion, not a fact.
 
In WWII, the Americans had more engineering resources than anyone else. The fact remains that the Mustang was designed mostly in a panic rush by people with limited experience in fighter design. It all worked out in the end, but it was not a good war strategy.

The Germans had their share of good aircraft and engine designers, but they missed the laminar flow wings and two-stage superchargers.
I was hoping Drgondog would have commented on this but here goes.
The Mustang started out as an in-house design, P.509. The P.509 was NAA Spec 1592, circa March 1940. This lead to the Mustang after the BPC went NAA to build P-40s for them.
"We got something better ".
My source on the P.509 information is THE SOURCE:
DrgonDog
In that light, I don't think the Mustang was that much of a rush job. Based on anecdotal evidence, I don't think "luck" had anything to do with it.
 
The fact remains that the Mustang was designed mostly in a panic rush by people with limited experience in fighter design. It all worked out in the end, but it was not a good war strategy.
The Mustang existed before the BPC approached North American.

This artwork is of NAA's P-509 project, rendered in 1940 - look familiar?
49-1-p-509-jpg.jpg


This image is from the P-509 thread that explains the genesis of the Mustang from NAA's drawing board to the NA-73 in good detail:

 
I don't think the P-51 was a stroke of "luck" but a product of nearly limitless resources, access to a skilled workforce, and maybe just as important, the space required and remoteness from the conflict to tinker with the design.
Its too bad somebody didn't smack Sydney Camm over the head with the NACA laminar flow research a little sooner, perhaps the Typhoon/Tornado could have been skipped, and introduced the Tempest and Fury a year or two earlier
 
We got lucky in that adding the Merlin to the Mustang proved not so troublesome, and gave us a LR fighter capable of tangling with almost anything.

With the Corsair, we got lucky in finding that the inverted-gull wing reduced drag at the wing roots, allowing the plane a higher turn of speed.

Perhaps the hard work and experience often result with a good luck?

I think it is also fair to say that the Americans got the benefit of what was happening in Europe, with regard to what the RAF and Luftwaffe were putting up in the skies in 1940. A Bf 109 and Bf 110 were shipped to the States in 1941, and I expect we also provided info on our own two fighters. What was discovered (and I know Vultee produced a comprehensive report and 20 minute film re the Bf 110) probably helped future thinking and development in some way. Which was no bad thing, given the ultimate performance of the US fighters in the last 12 months of the war over Germany, which was superb! And I say that as a Brit...

P-38 flew well before 1941. XP-47B was materializing in the winter of 1940/41, with engine and turbocharger system unavailable anywhere else bar USA. NA-73X (Mustang prototype) 1st flew in October 1940.
Probably neither Hurricane, nor Bf 109 nor 110 were offering anything to the Americans. With Spitfire it was another story, prompting NAA to see where the weight could be shed in quest that eventually produced the 'lightweight Mustangs'.
P-47 enjoyed the performance advantage vs. German fighters above 20000 ft for perhaps the last 20 months, and Merlin Mustang some 17 months.

What Americans failed to learn from the air battles of 1940-42 over Europe was that drop tank is a critical asset on an offensive fighter.
 
Perhaps the hard work and experience often result with a good luck?

Of course that's often the case. What hard work did the North American design team put in on the Merlin that made it so easy to adapt for the Mustang, though? I'm really at a loss why this point is being argued. It seems self-evident that someone asking "what if?" with something so complicated as an aero engine installation mod and having it work so smoothly is quite the lucky break.

This is not to say us Americans didn't do many things right; we did. It's just acknowledging that serendipity does sometimes happen.

 
Of course that's often the case. What hard work did the North American design team put in on the Merlin that made it so easy to adapt for the Mustang, though? I'm really at a loss why this point is being argued. It seems self-evident that someone asking "what if?" with something so complicated as an aero engine installation mod and having it work so smoothly is quite the lucky break.

This is not to say us Americans didn't do many things right; we did. It's just acknowledging that serendipity does sometimes happen.

'Merlinized' P-51 from NAA gained the deeper fuselage so the Merlin does not spoil the streamlining of the fighter despite the air tunnel under the engine (we can compare the Mustang X with XP-51B to see the more elegant lines of the later; IMO, granted, the only actual shortcoming of the Mustang X was that every Mustang I the RAF had was not converted into the Mk.X). They also reworked the cooling system from the one the Allison Mustangs had: lowered the intake so it is away from the boundary layer (also introducing the boundary layer splitter), oil cooler in the separate tunnel, intercooler radiator neatly housed together with coolant radiator. Engine power went up by a great deal, the drag probably remained close to the Allison Mustangs (otherwise the engine-related drag usually went up if an intercooled engine was introduced; certainly the engine drag was up in such case with Ta 152 and Spitfire).
 
I was hoping Drgondog would have commented on this but here goes.
The Mustang started out as an in-house design, P.509. The P.509 was NAA Spec 1592, circa March 1940. This lead to the Mustang after the BPC went NAA to build P-40s for them.
"We got something better ".
My source on the P.509 information is THE SOURCE:
DrgonDog
In that light, I don't think the Mustang was that much of a rush job. Based on anecdotal evidence, I don't think "luck" had anything to do with it.
There was a great deal of serendipity with the "birth" of the Mustang/P-51. Late enough to be able to incorporate the latest known technology in the final design but early enough to play a part in the war, but that isnt "luck". NAAs involvement with the British as a respected client and the British involvement with NAA as a responsible manufacturer played a huge part. It may be true that NAA had no "track record" with actual fighters, but they did have the T-6 Texan which the British bought and liked and was an education in mass producing such aircraft. I would also question the worth of "experience". The two companies with the most experience of making aircraft in UK made some of the biggest screw ups. Hawkers took an age to get the Typhoon sorted and Handley Page never got the Halifax to perform anything like a Lancaster.
 
I could be wrong, but I have been under the impression they were designed to allow for clearance for the large prop, and that the reduced drag was an ancillary benefit noticed later. I'm happy to be corrected if I am wrong. Getting good dope is why I read here.
The reverse gullwing also moved the wing away from the pilot, improving his view downward a bit.
 
Perhaps if luck was involved in the Mustang saga, it would be that the aircraft was as large as it was. That put it at a disadvantage occasionally against lighter aircraft, but it had the space to eventually carry far more fuel than originally envisioned
 
I've sat in many warbirds to include a Corsair, to be honest I don't think this made a difference
The Corsair's wing (width and area) were comparable to the F6F's, but the Corsair's cockpit was set back far enough, there was nothing that was going to help a pilot's view, short of putting windows in the wing.
 
Perhaps the hard work and experience often result with a good luck?



P-38 flew well before 1941. XP-47B was materializing in the winter of 1940/41, with engine and turbocharger system unavailable anywhere else bar USA. NA-73X (Mustang prototype) 1st flew in October 1940.
Probably neither Hurricane, nor Bf 109 nor 110 were offering anything to the Americans. With Spitfire it was another story, prompting NAA to see where the weight could be shed in quest that eventually produced the 'lightweight Mustangs'.
P-47 enjoyed the performance advantage vs. German fighters above 20000 ft for perhaps the last 20 months, and Merlin Mustang some 17 months.

What Americans failed to learn from the air battles of 1940-42 over Europe was that drop tank is a critical asset on an offensive fighter.
Go read the Vultee report...
 

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