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This thing about the Lanc being the least survivable keeps cropping up and seems to be just accepted by the statingof it, but why?
What says the Lanc could not absorb battle damage? The accounts I've read say exactly the opposite, that the Lanc could absorb astonishing amounts of damage and return home.
That does not place it in any kind of context against the B-17 and 24, but nor does is it even remotely imply any sort of vulnerability or fragility?
Does anyone have a any info on whether the B-17 or B-24 could climb and maintain formation with the main bomber stream/formation on three engines?
Are there any accounts of either of these types landing on one engine?
I do know there are accounts of the B-17 making it back to base with entire sections of the nose or tail missing, as there are with the Lanc too, but I'm wondering where this impression of fragility is coming from?
The pilots choice would appear to be the Lancaster,I read only yesterday ab account that said the B-17 'lumbered' into the air while the Lanc was eager to go, 'like a racehorse' even when fully laden, and supremely light and easy to fly, whilst also being manouverable (I think we've all heard of Henshaw Rolling it).
Regarding the lightness of control in flight, there was a great quote when a 5 foot 4 woman ATA ferry pilot was told by an RAF officer that he was amazed that she was going to deliver the squadrons new Lancaster single handed, she replied "Well sir, I am not proposing to carry it, I rather hope that it will be carrying me"
This thing about the Lanc being the least survivable keeps cropping up and seems to be just accepted by the statingof it, but why?
What says the Lanc could not absorb battle damage? The accounts I've read say exactly the opposite, that the Lanc could absorb astonishing amounts of damage and return home.
That does not place it in any kind of context against the B-17 and 24, but nor does is it even remotely imply any sort of vulnerability or fragility?
Does anyone have a any info on whether the B-17 or B-24 could climb and maintain formation with the main bomber stream/formation on three engines?
Are there any accounts of either of these types landing on one engine?
I do know there are accounts of the B-17 making it back to base with entire sections of the nose or tail missing, as there are with the Lanc too, but I'm wondering where this impression of fragility is coming from?
The pilots choice would appear to be the Lancaster,I read only yesterday ab account that said the B-17 'lumbered' into the air while the Lanc was eager to go, 'like a racehorse' even when fully laden, and supremely light and easy to fly, whilst also being manouverable (I think we've all heard of Henshaw Rolling it).
Regarding the lightness of control in flight, there was a great quote when a 5 foot 4 woman ATA ferry pilot was told by an RAF officer that he was amazed that she was going to deliver the squadrons new Lancaster single handed, she replied "Well sir, I am not proposing to carry it, I rather hope that it will be carrying me"
Those are good questions.
My guess is that its more of an assumption because its not heavily fortified like the B-17 was.
I can understand that larger planes are going to absorb more damage but flak was downing planes left and right regardless.
I know of one account where a B-17 did fly home on one engine, often two or three.
I might also broach the subject on the B-24 as having a laminar flow wing, if it hasn't already been mentioned. I'm not sure which variant but its worth noting.
I was reading up on laminar flow and it mentions its discovery well before they ever made a wing intended to have laminar flow. In fact, the P-51s laminar flow may not have been so laminar after all, as defined by what laminar actually means, but it did have a wing that reduced drag over the wing.
Bill
Did it though?The Lancasters manouverability did directly contribute to its survivability due to manouvres such as the corkscrew etc which saved many lives and which other bombers, and here's the crucial point were not *strong enough* to replicate to anywhere near the same degree.
Which brings me back to the main thrust of my original question, can it actually be quantified in ay way that the B-17 could absorb more battle damage structurally? I would not go so far as to say the Lancaster was stronger than the B-17, but can it be shown that it was weaker?
Did it though?
With both the USAAF and the RAF facing heavily cannon-armed opposition, the point of structural survivability is a largely academic one.
The point there is that second crewmember going to be proficient enough to perform in the same capacity as the assigned pilot? Additionally the second crewmember isn't along side the pilot the whole time, sharing the workload and relieving some of the operational stress. Lastly that's where the extra set of eyes come into play.The single pilot argument is also clear enough, although there was always at least one other crew member capable of taking over from the pilot so it was not not quite as terminal a problem as it might appear.
In the end I think it would be a matter of where and when the damage to the aircraft occurred and how absorbed. There is no doubt that a radial engine will out survive and inline. Additionally one would have to look at how the aircraft performs with engines out and parts of the airframe shot away. As mentioned earlier the B-24 was a handful when one or more engines were gone or if there was damage to the wings. I've heard of stores (and seen photos) where pieces of B-17s were shot away and the pilots saw little or no change in performance.The Lancasters manouverability did directly contribute to its survivability due to manouvres such as the corkscrew etc which saved many lives and which other bombers, and here's the crucial poin' were not *strong enough* to replicate to anywhere near the same degree.
Which brings me back to the main thrust of my original question, can it actually be quantified in ay way that the B-17 could absorb more battle damage structurally? I would not go so far as to say the Lancaster was stronger than the B-17, but can it be shown that it was weaker?
Don't misunderstand meEven if greater structural strength only saved 20% of cannon-struck bombers that might have otherwise not returned, I'd still consider it significant.
How can this survivability-through-manoeuverability be quantified?
If Lancasters did have ventral turrets, how much better do you think they would have fared against Schrage Muzik-configured nachtjaegers?
The point there is that second crewmember going to be proficient enough to perform in the same capacity as the assigned pilot? Additionally the second crewmember isn't along side the pilot the whole time, sharing the workload and relieving some of the operational stress. Lastly that's where the extra set of eyes come into play.
In the end I think it would be a matter of where and when the damage to the aircraft occurred and how absorbed. There is no doubt that a radial engine will out survive and inline. Additionally one would have to look at how the aircraft performs with engines out and parts of the airframe shot away. As mentioned earlier the B-24 was a handful when one or more engines were gone or if there was damage to the wings. I've heard of stores (and seen photos) where pieces of B-17s were shot away and the pilots saw little or no change in performance.
Not really - in the USAAF usually the Navigator or flight engineer could fly as well and at least one FE did manage to land a crippled B-17 and got the MOH for it. The chances of pilot incapacity were very slim - the fact that a single pilot could make twice the mistakes when flying a 4 engine aircraft is the point, and I remain that there would have been a lot less lancaster losses if they were flown with a dedicated co-pilot, and that's not taking anything away from the plane or the crews that flew her.Another thought occurs. In one way (and on rare occasions) might the RAF way have been better? In the Lanc a 'semi trained' pilot could climb into the cockpit if the pilot was hit, and take the plane home, but in a direct hit on a B-17 cockpit that incapacitates both pilots, what would happen?
As reliable as the Merlin is/was, it still carries a coolant system and is a lot more vulnerable than a radial hands down. The point is a radial can be shot to pieces and still work. You ain't flying with pistons missing from a Merlin...I dont think the durability of a radial engine is particularly relevant for a four engined plane that can fly quite happily on two, especially two of the most reliable and durable inlines in history.
The Lancaster for the most part had little or no faults in its operational career and it was the perfect bomber at the perfect time, but technology quickly eclipsed the aircraft as it quickly disappeared from front line squadrons at war's end and those that survived saw many years in secondary roles. IMO it was the best heavy bomber of the European Theater.I believe the biggest failing in the Lancaster was the aforementioned lack of a belly turret, which was the result of official policy decisions as Avro had designed it with one. I don't think it can be faulted in any other area, except for the only toilet being right at the back, meaning the pilot was out of his seat for longer than necessary (though many resorted to taking a po with them)
Somewhere on here I seen that lancasters had high weather related losses or losses during landing, but I don't think specifics were given. It would be at that time where this should be the most prevalent.We would have to see how many otherwise flyable aircraft were lost due to the loss of the pilot to prove that, but I wouldn't know how to go about it. Common sense says that it must have happened, but was it a significant number?
Try operating any in line engine without coolant. Heads and head gaskets don't do well...I do agree on the radial v inline engines point, but I just feel that to lose the power or coolant for three of your four engines would be extremely unfortunate, and you would probably have other problems with that many hits in close proximity. Interestingly, the radial powered Lancaster II had lower performance and was generally disliked in comparison to the Merlin Lanc. Production of this model ended after only 300 had been built
I agree with your last paragraph. If anything the Lancaster was the ultimate expression of pre-war bomber technology. The B-29 was the future and it had its equivalents on the drawing boards of Avro, Handley Page and Shorts, but once the war began there was no way British industry was going to be allowed to pursue such lengthy, expensive and risky development paths. Did you know there was a move during 1943-44 to have an anglicized B-29 built in the UK for the RAF, but the length of time it would take to put bombers into service meant it was dropped, only for us to have to buy 2nd had ex USAF 'Washington's ' in 1950.
Each engine had its own supply.This might seem a rather basic question, but Im no engineer, was there just the one single coolant tank for all four engines, or did each have its own supply?
Almost right on the Lancaster II, it was built in anticipation of a shortage of Merlins that never actually materialised, but so great was the loss of performance that it was dropped ASAP. In contrast to this the Halifax III (Hercules radial) was vastly superior to the Merlin Halifax, but still inferior to the Lancaster I.
In the spring of 1943 Ralph Sorley (after evaluation of several new designs) nominated the B-29 as ' the only prospective short term replacement for the Lancaster'. Discussions to this end were led by Lord Portal and a delegation travelled to the US to discuss it. Alas my source lacks any fine detail and concludes only with the statement that 'the problems in adapting the type for night bombing from England proved insurmountable in the time available and so the type was never used'
Any further specifics on this from anyone who has them would be welcome
WayneThis might seem a rather basic question, but Im no engineer, was there just the one single coolant tank for all four engines, or did each have its own supply?
Wayne
look at it this way
think how utterly stuffed all four engines would be if a sole coolant reservoir was perforated
That's a big glider...
The Lancaster had a service ceiling of 24500, the B24 had a service ceiling of 28000 feet, the B17 had a service ceiling of 35000 feet. Which was most survivable against the heavy bomber's arch enemy, Flak?
The Lancaster had a service ceiling of 24500, the B24 had a service ceiling of 28000 feet, the B17 had a service ceiling of 35000 feet. Which was most survivable against the heavy bomber's arch enemy, Flak?