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I have long ago learned they were Allisons. However, at that time, she asked me what I was thinking about. I made the B-17 / Merlin statement. I just want to be honest.Not Merlins... Allison V-1710-89 engines.
The XB-38 delivered a higher top speed, but its ceiling was lower. After a few flights it was grounded due to exhaust gas leaks from the engine manifolds. Once this had been fixed, testing resumed until the ninth flight on June 16, 1943 when the inboard starboard engine caught fire and the crew bailed out. The XB-38 was destroyed and the project was canceled, in part because the V-1710 engines were in high demand for P-38, P-39, & P-40 fighters (by mid-1943 the P-51 was only produced with Packard Merlins).
XB-38:
max speed 327 mph (526 km/h, 284 kn) at 25,000 ft (7,600 m)
cruising speed 226 mph (364 km/h, 197 kn)
service ceiling 29,600 ft (9,020 m)
B-17F (type in production in June 1943):
max speed 299 mph* (481 km/h, 261 kn)
cruising speed 200 mph (322 km/h, 176 kn)
service ceiling 37,500 feet
* 325 mph War Emergency Power for short periods
A recent interview revealed that that some also do not want their boyfriends to be "one of the boys" either. Don't ask me what that means.They also do NOT want to be "just one of the boys". Ask me how I know.
service ceiling 29,600 ft (9,020 m)
When the early models of the P-38 came out they had a problem with the turbos overspeeding at high altitudes and that is where the shield to protect the pilot from the turbos exploding came from. They corrected that by increasing the boost out of the engine driven supercharger by changing the gear ratios and they probably could have upped the boost on the XB-38 the same way. Aside from that, they no doubt used the original air-to-air intercoolers inside the wings. If they had switched to use air-to-liquid intercoolers such as the Merlin Mustang employed they likely could have reduced drag.Service ceiling 37,500 feet
Aside from that, they no doubt used the original air-to-air intercoolers inside the wings. If they had switched to use air-to-liquid intercoolers such as the Merlin Mustang employed they likely could have reduced drag.
He means that the engine Nacelles are at right angles to the Wing, not aligned so to be parallel with a vertical line coming up 90 degrees to the ground. The dihedral of the wing makes the difference.I just read your post with interest. Can you clarify what is meant by aligning the nacelles vertically?
Ahhh that's really interesting. Very few aircraft go against the general concept. Junkers Ju-52 for example, has its engines mounted to perpendicular to the leading edges of the wing, rather than parallel to the line of flight.He means that the engine Nacelles are at right angles to the Wing, not aligned so to be parallel with a vertical line coming up 90 degrees to the ground. The dihedral of the wing makes the difference.
I loves me my shark tails. I'd love to see the 299.
Saparo:I loves me my shark tails. I'd love to see the 299.
Tbird:Skye, I think you may have misunderstood the comment about the B-29 engine alignment. When viewed from above, the nacelles are indeed aligned with the direction of flight, like almost all aircraft. Like you said, the Ju52 was an oddball, having the engines pointed outwards, perpendicular to the leading edge sweep angle. Strangely, the Fw200 outer engines were also pointed outwards.
The point I was making about the B-29 and XB-39 is that when viewed from the front, the oval-shaped nacelles are not oriented vertically relative to the ground. They are tilted by the amount of the wing dihedral. The 1/72 Academy B-29 model orients the nacelles vertically, so it is incorrect. Not all that noticeable on a B-29. I had to go look at a real B-29 to convince myself about this as it was kind of hard to tell in photos. It is far more obvious on the XB-39 with those huge nacelles, however. The great thing about this from a modeling perspective (and maybe for the Boeing engineers who designed the B-29) is that it makes the port and starboard sides more similar.