Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules
That was my point regarding why the B-32 did Not have a pressurized tunnel similar to B-29.The B-17 and B-24 far as I know have passage ways between the forward and rear compartments. The catwalk over the bomb-bay on those planes does the job
Because the B-34 was pressurized and the others were not. Without a tunnel you would have to depressurize both areas to allow anyone to travel between.So tell me again why B-32 needs a tunnel? for same design altitudes as B-24 and B-17 - which did not have tunnels?
Obviously infrared sensors are off the table, but were airborne-capable optical sights of the time good enough? Radar-directed options as well perhaps?
Putting a big airframe low to the ground and at high speeds repeatedly tends to weaken the airframe a bit. Fatigue might become an issue. The B-32's wing was designed for high altitude, not low altitude. Vibration could set in, throwing the pilot's aim, all manner of things might happen. Unless trials were done it would be impossible to say exactly what might or might not work.
Hence why I was wondering if making it a predecessor of the AC-47 gunship might have worked,
agreed though for the first couple of days the gunners would have been confused by the size and especially speed and screwed up their lead allowances. Lead as in angle not lead as in weight (gosh I love English with its same word totally different meanings)
Did the technology exist in 1945 to turn a B-29 or B-32 into a AC-130 style gunship? Obviously infrared sensors are off the table, but were airborne-capable optical sights of the time good enough? Radar-directed options as well perhaps?
The interesting thing is both the B-1 (Bone) and the B-52 (Buff) became quite useful for Close Air Support (CAS) in Afghanistan. Hours and hours of loiter time, unbelievable amount of weapons (Precision Guided Munitions AKA PGMs), air refuelable. The grunts loved having hours of hate circling above them ready at a moments notice.
Cheers,
Biff
I'm surprised it took so long to be introduced to operational use. It's first flight was around the same time as the B-29.Why? Its operating altitude was much lower than B-29 and B-29 ops from March 1945 to EOW showed that high altitude ops were less effective over Japan than traditional ETO ops.
I'm surprised it took so long to be introduced to operational use. It's first flight was around the same time as the B-29.
Cowling-flap design: If I recall the position of the cowl-flaps had a serious effect on the plane's cruising speed. I'm not sure if there was anything unusual about the cowl-flaps or simply due to the plane being underpowered.
From what I understand, B-29s taking off from shorter than ideal runways on their island bases while being overloaded had to carefully set the cowling flaps so that the engine did not overheat and the drag was low enough that the required take-off speed could be reached before the end of the runway.
So would the USAAF have purchased the engines from Britain (assuming that the British had any to spare) or would the U.S. have had to tool up a manufacturing plant (like Packard did) and make their own.After a lot of research on the topic, I've long since come to the conclusion that the R-3350 of WWII was an absolutely execrable engine in all aspects. In fact, it wasn't until a complete redesign of the engine after WWII that it could be considered useful vs dangerous. And that was due to Chrysler's work on the engine.
I have often wondered what might have been the case if the USAAF had not been so US-centric and used the Bristol Centaurus "bomber engine" on both the B-29 and the B-32. I suspect that both aircraft would have been substantially safer and earlier in their combat usage had that been the case.
AlanG
Much more likely would have been to use the Allison V-3420. While the Centaurus was a great engine, I don't think it would be available in timeAfter a lot of research on the topic, I've long since come to the conclusion that the R-3350 of WWII was an absolutely execrable engine in all aspects. In fact, it wasn't until a complete redesign of the engine after WWII that it could be considered useful vs dangerous. And that was due to Chrysler's work on the engine.
I have often wondered what might have been the case if the USAAF had not been so US-centric and used the Bristol Centaurus "bomber engine" on both the B-29 and the B-32. I suspect that both aircraft would have been substantially safer and earlier in their combat usage had that been the case.
AlanG
Much more likely would have been to use the Allison V-3420. While the Centaurus was a great engine, I don't think it would be available in time