Simon Thomas
Senior Airman
For those of us who are a little dim, could someone please explain (preferably using small words) why all the planes on the missions had to be interchangeable?
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So there would be no down-time in the event the primary bomber was unable to go on the mission.For those of us who are a little dim, could someone please explain (preferably using small words) why all the planes on the missions had to be interchangeable?
Is that so much to ask for?Oh, he'd just build an asymmetric canard with five engines
The Horton Ho.XVIII was betterIs that so much to ask for?
(2) Sigh... that's the maximum cruise speed!!!! See:
I've already shown that econ cruise for a Grandslam Lancaster was 212mph TAS at 15K ft at 4.5lb boost at 2650RPM.
If the B-29 and the B-32 had failed, the US didn't have a second fallback: neither the B-17 nor B-24 could have carried the nuclear bombs of 1945.
Keep yer hair on. Looks like it is, in translating the data into the book must have missed that. Doesn't really change the premise of what I posted though and my original position still stands, the B.I (Special)s had lower performance than the unmodified B.Is as a result of extra weight despite more powerful engines and more effective propeller blades.
Yup, but at 15,000 ft, which is just ridiculous over Japan in 1945. You're gonna want AT LEAST 20,000 feet with a cruise of around 200 mph plus. So, the B.I (Special) still can't do that.
Nothing has changed despite your correction. You are still not going to get the range figures WITHOUT in-flight refuelling, not at the performance and altitude that is necessary.
Fat Man was dia 1.5m x 3.3m long so with an area of 1.766 sqm. I suspect a Cd of about 0.1 which would degrade to 0.2 if half in the slipstream.
at 120m/s speed an air density of about 0.4kg/cubic meter seems to generate about 1272 newtons of drag that would take 152kW (about 200hp) to overcome. The drag is probably about the jet thrust one of the merlin's was producing. The engines are at about 1/2 power (so a total 4 x 1000Ho=4000hp) so we are loosing 5% maybe 10% so with a cubed law we are going to loose about 1.8% speed. Very rough calculation. I could be off by 100% in which case the speed drop is more like 3.3% (12 mph) about the same as turret deletion would gain.
Deleting the rather big dorsal turret compensates for Fat Man in a distended streamlined belly.
These numbers are based upon the Operation Catechism Lancasters that had ~2550IG of internal fuel. a 12000lb Tallboy, and were Lancaster Is refitted with Merlin 24 engines.
Merlin 24 TO HP = 1610 / 1510HP at 9.250K ft
Merlin 85 TO HP = 1635 / 1680HP at 16K ft
Merlin 86 TO HP = 1605 / 14400HP at 22.25K ft
A FATMAN bomb in a modded bomb-bay, with both forward turrets removed is likely to be little different from an unmodded Lancaster VI, in terms of drag and thus speed:
Which bear no reality to the operation being planned here. Firstly, as it has been pointed out to you, altitudes below 20,000 feet over Japan in 1945? REALLY? As soon as you go higher your performance decreases and if you want to increase it, that chews into your fuel reducing your range. Next, the conditions in Northern Europe are very different to the Pacific theatre, which, it has already been pointed out to you would affect the aircraft's performance, so again, these figures as flown during Catechism wouldn't apply.
As for the Lancaster VI, again we run into problems regarding the modifications you intend to make to this aircraft, which would reduce its performance further, so the standard figures as stated on that sheet you continuously promote as evidence the Lancaster could do the raid WOULD NOT APPLY (How many times does this need to be pointed out to you?).
Sigh, the ONLY way this raid could be carried out by a Lancaster, regardless of what mark it is, is with in-flight refuelling. If not, you might as well get a Whitley to do it. It would be less of a waste of a good aeroplane.
"Welcome to Fantasy Island!"
Members take the time to work on complex problems to derive meaningful results and this is your reply...
Where have I ever stated that they would be cruising over Japan at less than 20K ft? Why do you keep repeating this? Can you not read the performance charts for the Lancaster VI?
Aaand here is a classic example. Standard figures for the Lancaster VI wouldn't apply. You have indicated that your Lancaster VI needs modifying with fuel tanks in the bomb bay and the weight of the bomb itself, to increase its range. In order to do this you'll need to strengthen the bomb bay, the undercarriage and remove turrets to reduce drag, but performance is going to be considerably reduced and since you keep insisting without evidence that it can carry a Fat Man, the drag penalty would be severe, to say nothing for the impact on the handling. Add to that the Pacific conditions and your Lancaster is not going to achieve the figures you keep promoting... FANTASY ISLAND my friend. The only way you can do it is with in-flight refuelling.
(1)The fact is YOU DON'T KNOW what the Lancaster VI's figures would be with all these mods you talk about, so the only thing we can go on is by applying what we know about B.I (Specials) and how the modifications applied affected those, because, as you have said yourself, both the B.I (Specials) and Lanc VIs are just B.Is, which we know COULD'NT do the raid WITHOUT substantial modification.
None of this is rocket science and you should be able to follow it, and if you can't...Fat Man was dia 1.5m x 3.3m long so with an area of 1.766 sqm. I suspect a Cd of about 0.1 which would degrade to 0.2 if half in the slipstream.
at 120m/s speed an air density of about 0.4kg/cubic meter seems to generate about 1272 newtons of drag that would take 152kW (about 200hp) to overcome. The drag is probably about the jet thrust one of the merlin's was producing. The engines are at about 1/2 power (so a total 4 x 1000Ho=4000hp) so we are loosing 5% maybe 10% so with a cubed law we are going to loose about 1.8% speed. Very rough calculation. I could be off by 100% in which case the speed drop is more like 3.3% (12 mph) about the same as turret deletion would gain.
Deleting the rather big dorsal turret compensates for Fat Man in a distended streamlined belly.
And what happens when there's a monsoon that causes the first leg of the mission to be flown at 17,000 instead of 9,000 feet?Again, (how often do I have to repeat this?) the aircraft will burn off ~11000lb of fuel during the low altitude, overwater, cruise before beginning the climb to combat altitude, which will burn another ~4000lb of fuel so that at the beginning of the bomb run, aircraft weight will be ~55000lb.
And what happens when there's a monsoon that causes the first leg of the mission to be flown at 17,000 instead of 9,000 feet?
The fleet of Mk.VI Lancasters totaled a number of 9.
Nine ships in that version says volumes. You're casting your lot on a type that saw limited service, did not distinguish itself like the other marks, had a history of maintenance issues all for the sake of insisting it could somehow match the performance of the B-29 on two missions that were, for it's time, incredibly sophisticated.
Please, give it a rest. It wasn't going to happen, no matter how you spin the numbers...
I have to say, your retro-vision is remarkable.
If only the leaders and commanders had a fraction of your knowledge, the war would have turned out quite differently.
Ramsey had a lot more knowledge than me which is why he recommended the Lancaster.