I've read a bit about the He 177: It's one of those completely absurd designs that leave you scratching your head. While many unorthodox designs have been proposed: Most are weeded out before they ever fly. While there are others that manage to proceed, there are the very small number that make the unorthodox work (such as the de Havilland Mosquito); most, however, are heavily-modified in either, the design-stage, or the flight-test phase.
While some of it's specifications weren't all that unreasonable, the requirement for moderate-angle (40-50 degree) dive-bombing attacks was a rather unusual feature. It would require considerable strengthening to the fuselage, as it would require stronger wings and fuselage, as well as the ability to tolerate higher maximum airspeeds than normally required for a heavy-bomber; while, I'd almost swear, I heard that the Royal Air Ministry's P.13/36 specification (gave rise to the Avro Manchester) demanded some steep diving requirements too, they were reduced to a more reasonable 25-30-degrees (still impressive for a heavy-bomber): The RLM actually demand these requirements to be increased to 60-degrees, something that required dive-brakes, an additional degree of strength (and weight), and reduced overall range (even with additional fuel), and a more complicated main landing-gear arrangement to support it (that said, I'm not sure if it posed any reliability issues).
That said, some of the design features weren't entirely the fault of the RLM. Some were Heinkel's fault as well, either through personal preferences, or responses to the changing requirements. For starters, they had a strong predilection to the idea of surface evaporative cooling (something which works well for race-planes, but not combat aircraft), and also chose the DB606 (which wasn't an RLM requirement) with the hope of reducing installation drag by 3%.
While the DB606 wasn't intrinsically flawed (it worked on the He 119 and Me 261), the idea of using surface cooling on the DB601 was impractical (it'd work, but the plane could be easily incapacitated by a few well-placed rounds). With the DB606, it was damned-near impossible. In an effort to keep cooling drag down, they used a tight-cowl, which made sense, but the engine ran quite hot, and tight cowls tend to produce inadequate cooling at certain speeds. Given that a hotter engine produces hotter exhaust, and the DB606's inner exhaust ducts run close to each other, have less ambient air flowing around them, they produce high temperatures and deposit soot, which can ignite.
The increases in weight resulted in the engine installation being recessed further back inside the wings without a firewall. The oil pump was badly designed, and the position of the electrical harnesses and oil lines, all served to make fires occur easily. Without a firewall installed, the airplane could quickly go up.
It's pretty obvious with 20/20 hindsight (or the properly calibrated crystal-ball -- thanks, X XBe02Drvr -- that's become one of my favorite expressions) that the Lotfernohr 7 bombsight would come online in 1941, and the dive bombing requirement would be lifted in 1942: The fact is that the Do 17/215 & Ju 88 were predominantly level-bombers that could do dive-bombing if need be. The moderate-angle dive requirement prior to late 1937 was probably already overkill, but it might have been easier to achieve weight and range requirements.
It seems 4 x DB601 would be the best choice because it'd have a smaller propeller diameter, and that'd simplify the landing-gear. I remember hearing that drag difference would be all of 3%, and that could be covered by some aerodynamic refinement.
While some of it's specifications weren't all that unreasonable, the requirement for moderate-angle (40-50 degree) dive-bombing attacks was a rather unusual feature. It would require considerable strengthening to the fuselage, as it would require stronger wings and fuselage, as well as the ability to tolerate higher maximum airspeeds than normally required for a heavy-bomber; while, I'd almost swear, I heard that the Royal Air Ministry's P.13/36 specification (gave rise to the Avro Manchester) demanded some steep diving requirements too, they were reduced to a more reasonable 25-30-degrees (still impressive for a heavy-bomber): The RLM actually demand these requirements to be increased to 60-degrees, something that required dive-brakes, an additional degree of strength (and weight), and reduced overall range (even with additional fuel), and a more complicated main landing-gear arrangement to support it (that said, I'm not sure if it posed any reliability issues).
That said, some of the design features weren't entirely the fault of the RLM. Some were Heinkel's fault as well, either through personal preferences, or responses to the changing requirements. For starters, they had a strong predilection to the idea of surface evaporative cooling (something which works well for race-planes, but not combat aircraft), and also chose the DB606 (which wasn't an RLM requirement) with the hope of reducing installation drag by 3%.
While the DB606 wasn't intrinsically flawed (it worked on the He 119 and Me 261), the idea of using surface cooling on the DB601 was impractical (it'd work, but the plane could be easily incapacitated by a few well-placed rounds). With the DB606, it was damned-near impossible. In an effort to keep cooling drag down, they used a tight-cowl, which made sense, but the engine ran quite hot, and tight cowls tend to produce inadequate cooling at certain speeds. Given that a hotter engine produces hotter exhaust, and the DB606's inner exhaust ducts run close to each other, have less ambient air flowing around them, they produce high temperatures and deposit soot, which can ignite.
The increases in weight resulted in the engine installation being recessed further back inside the wings without a firewall. The oil pump was badly designed, and the position of the electrical harnesses and oil lines, all served to make fires occur easily. Without a firewall installed, the airplane could quickly go up.
It's pretty obvious with 20/20 hindsight (or the properly calibrated crystal-ball -- thanks, X XBe02Drvr -- that's become one of my favorite expressions) that the Lotfernohr 7 bombsight would come online in 1941, and the dive bombing requirement would be lifted in 1942: The fact is that the Do 17/215 & Ju 88 were predominantly level-bombers that could do dive-bombing if need be. The moderate-angle dive requirement prior to late 1937 was probably already overkill, but it might have been easier to achieve weight and range requirements.
It seems 4 x DB601 would be the best choice because it'd have a smaller propeller diameter, and that'd simplify the landing-gear. I remember hearing that drag difference would be all of 3%, and that could be covered by some aerodynamic refinement.
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