Aces High Bulletin Board
General Forums => Aircraft and Vehicles => Topic started by: Wolfala on October 02, 2006, 01:22:46 PM
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I was doing some poking around, and apparently Allison made a late model V-1710 as a turbo-compound engine, rated at 2320 HP, and over 3000 HP with WEP.
(http://www.pilotfriend.com/aero_engines/images/turbocompound.jpg)
Was it too late in the war to see a re-engined P-38 or P-40 with one of these?
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Considering it looks like it's twice as long, I don't think a simple re-engine would suffice, I think a redesign would have been required of the airframe it was placed on.
That's what my uneducated guess would be.
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looking at a P-40e cutaway looks like it would all fit without moving to pit back, but i bet you'd be out of gas in about 20 min...it should go in a Mustang
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IIRC it was experimentally fitted to a P-63 but never flown.
gripen
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Originally posted by gripen
IIRC it was experimentally fitted to a P-63 but never flown.
gripen
XP-63H
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O well. One can always salivate at the prospect of a P-38 with 6000 hp in a climb. Or going into compression in level flight.
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Originally posted by Wolfala
O well. One can always salivate at the prospect of a P-38 with 6000 hp in a climb. Or going into compression in level flight.
The P-38K could probably come close to compressing in level flight. Carried to the next logical progression, as in being fitted with FOUR blade paddle props and the later 2000+HP Allisons (the next logical progression of the 1875HP F-15 series engines that were in the P-38K), you could probably reach the limits of the airframe without great difficulty, given the performance of the P-38K prototype. It'd damned sure be a fun bird to play with.
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Put it in a Spitty. Mk VIII airframe, clipped :D
ROC 7500 fpm?