Most agile four engined aircraft ww2?

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The B-36's wingspan is literally the length of a city block, so yeah, it's going to require six engines and four boosters.

The Huges H-4 (Spruce Goose) had eight engines.

The BV238 had six engines.
You cant look good with so many though
 
The Martin P4M Mercator came with two jets built into the rear of the piston nacelles, so a 4 engine,2 turning ,2burning from the start.

In 1960 at W.Pat, the B-36 was on outside unrestored display. A USAFA cadet looked (with a boost up) in a waist blister and seeing the bunks of the relief crew section, exclaimed, "It's a flying whore house."
 
Or the YB-60.
The YB-60's range was short of 3,000 miles compared to the B-36's range of 10,000 plus it's max. lift was the B-36's standard load of 72,000 (the B-36 max. load was about 87,000 pounds for shorter ranged missions).

It would be interesting to see how turboprops would have enabled the Peacemaker to retain it's piston-powered range/load profile while increasing speed.
The Tu-95 has a range of about 9,300 miles, though it's much smaller.
 
The YB-60's range was short of 3,000 miles compared to the B-36's range of 10,000 plus it's max. lift was the B-36's standard load of 72,000 (the B-36 max. load was about 87,000 pounds for shorter ranged missions).

It would be interesting to see how turboprops would have enabled the Peacemaker to retain it's piston-powered range/load profile while increasing speed.
The Tu-95 has a range of about 9,300 miles, though it's much smaller.

According to the Standard Aircraft Characteristics for the B-36B, the combat radius with maximum bomb load (86,000 lbs) was 1,757 nautical miles. That was with an initial cruising altitude of 10,000 feet, and a final cruising and bombing altitude of 25,000.

With a 10,000 lb bomb load and a final cruising and bombing altitude of 40,000 feet, the combat radius was 3,500 nautical miles.

Source.
 
Eric Brown's take on the He 177 is worth examining for perspective. He said that its climb was ponderous and in flight the aircraft was sensitive to turbulence, but he found that stability was positive in all axes, but that control sensitivity was high for such a large aircraft, believing the elevator to be dangerously light. When performing diving trials, at a 400 km/h dive the aircraft handled well, and control responsiveness was good, particularly in the elevator, which might explain its sensitivity, although he remarked that aircraft had suffered structural failure in flight so he was very careful with not over exerting use of the elevator.

As a dive bomber, Brown stated that it was vital to know the exact weight of the aircraft before making diving attacks, with pull-out acceleration of 2.3G and a weight of 27 tonnes, this was extremely important. The aircraft had an automatic pull-out device, but, in his word, "...it really was somewhat nail-biting to have to treat a giant like this immense Heinkel bomber as though it were made of glass", concluding that "...dive bombing in a Junkers Ju 87 was one thing, but in a monster like the He 177 it was little short of ludicrous."

He states that the stalling characteristics were mild with pronounced buffet at 185 km/h (115 mph) and with the undercarriage lowered it buffeted violently at 140 km/h (87 mph), which led Brown to fear the aircraft had suffered structural damage. Landing roll was lengthy and the aircraft showed no desire to want to slow down, heavy braking inducing excessive judder and a tendency for the aircraft to swing as it slowed down. Brown believed the brakes were too inadequate to slow it and with the very real threat of ground looping the aircraft, knowing that it had undercarriage difficulties, plus the delicate handling in flight, led him to thinking it was far too fragile handling-wise for an operational bomber. Retrospectively he stated that during his career he really enjoyed test-flying the numerous German aircraft he flew, but with one exception, the He 177.
Interesting memories from someone with first hand experience. It confirms that the base design was promising but implementation suffered from some bad decisions, taken outside of Heinkel's offices.
 
It confirms that the base design was promising but implementation suffered from some bad decisions, taken outside of Heinkel's offices.

Agree in principle but Heinkel is not entirely blameless. Take a look at the post before the one you linked to, some of those things that the aircraft suffered are entirely Heinkel's doing.
 
Four-engined beauty contest?
(demonic laughter in the background)
far5.jpg
 

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