Out of the Big Three WW2 bombers (B-17, B-24, Lancaster), was the Flying Fortress the most redundant?

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Well it is often described as the looking like the crate the B-17 came in! But beauty is in the eye of the beholder. Adding the front turret did nothing for it aesthetically but was a vast improvement defence wise.
To me, the front turret B-24s are more aesthetical than the earlier models, but the eye of the beholder.
 
A few notes if I may.
The B-17 was originally sold as hemisphere defence carrying the 1,600 AP bombs against approaching ships,
The time line doesn't work for this.
The 1600lb AP bomb only came into service in May of 1942.
They may have been fooling around with the design for a number of years?
There were five different AP bombs ranging from 600lbs to 1400lbs that are older.

The US was using 600lb GP bombs as standard in the 1930s At the time the Y1B-17s intercepted the Rex (May of 1938) The official bomb load was eight 600lb bpmbs.
Miss print or a bit of creative writing?
They were being sold as hemisphere defence, just not with 1600lb bombs.
BTW the Y1B-17s only had 930hp per engine at this time and the turbos would not be installed until until the last Y1B-17 was built and delivered in Jan 1939.
640px-B-17s_flyby_Rex.jpg

the B-24 was meant as a heavy bomber, not a B-17 replacement but a second design in production.
That it was but both the B-17 and the B-24 were evolving.
The original XB-24 did not have turbo chargers or power turrets, and grossed under 40,000lbs.
The original XB-24 also missed it's predicted speed of 311mph and only managed 273 which was rather below what the B-17C (with turbos) could manage.
Consolidated went to work figuring out how to install turbos but in the meantime the French and British got the slots on the production while the AAC waited for the "improved" planes. The modified XB-24 was flown with turbos on Feb 1941, in the mean time, the French had ordered 60 B-24s with an option for 120 more and the British had ordered 164 more.
USN PB4Y-2
I Believe the PB4Y-2 did not have turbocharges which makes comparisons of ranges and speeds a little difficult as they were flying at different altitudes?
 
"The B-24 bomber one of the most difficult planes to fly during WWII. It was unpressurized, underpowered and prone to explode on takeoff. Unlike the B-17, the B-24 could not maintain altitude if one engine was lost. If two engines were lost, the plane would drop pretty much like a rock." B-24 NAVIGATOR HARRY FORNALCZYK

What about the "Liberty Lad" which participated on Operation Tidal Wave and came back with two engines lost on one side(!) after an 16 hours flight?
"...drop pretty much like a rock." sounds like a bit of an exaggeration.
 
The 'single tail' B-24N was always intended as the definitive B-24.
It had been test flown in 1943 as the XB-24K, demonstrating superior handling, climb and speed - it cruised 30mph faster than a B-17 while carrying a much bigger bomb load.
It became a very substantial redevelopment of the basic B-24 into almost a new aircraft. Production was ramped up for commencement in mid 1945 at Willow Run, but the end of the war saw the order for 5,160 cancelled.

XB-24K

View attachment 666150


B-25N
View attachment 666151
Why did the single tail work better?
I thought a twin tail is suited to be more in the airstream of the engine blade (2 engines and more) and thus provide more control.
Maybe someone can explain it from aerodynamical view.
 
The B-17 wasnt what the USA wanted but it was pretty much the only game in town, so it was ordered. The B-24 was ordered to have more range payload and altitude which is a big ask with the same engines, it didnt succeed in all that but extra range and payload made it complimentary, if it wasnt better in many/most respects it wouldnt have been made at all. Consolidated would have been building B-17s. What the US wanted was a B-29 or similar but you cant design and build a plane without the engines to power it and the B-29 engines were the next generation, So the US did the logical thing, you pee on the pot that you have until a better pot is available. If they hadnt and waited and waited, they wouldnt have had an airforce in 1944 and the whole of WW2 would have passed them bye.
 
Can we all agree though: the B-24 was an ugly aircraft! If pigs could fly, they'd look like B-24s.
NOT TRUE!
It's the coolest-looking heavy, ever! The long, slender Davis wing with its distinct airfoilprofile, the unmistakable oval twin tail and the contrasting cumbersome, flabsided fuselage with a dog-snout (with turret) give it a unique appearance. It is COOL!
The B-17 is a boring stereotypical prom queen. The Lancaster is a flying hunchback.
 
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NOT TRUE!
It's the coolest-looking heavy, ever! The long, slender Davis wing with its distinct airfoilprofile, the unmistakable oval twin tail and the contrasting cumbersome, flabsided fuselage with a dog-snout (with turret) give it a unique appearance. It is COOL!
The B-17 is a boring sterotypical prom queen. The Lancaster is a fling hunchback.
It was a pregnant glider, it should have been made from girders, painted blue and never allowed in the air, like that stuff from Grumman.
 
The early (around 1940 to early 1941 ) B-17s and B-24 were around 40,000lb planes that they were running overloaded.
the B-17E showed up in Nov 1941. weights were
Weights: 32,350 pounds empty, 40,260 pounds gross, 53,000 pounds maximum. Much like some of our ideas for escort fighters the intent was to burn off a lot of the fuel before the planes got into combat. That and use lighter bombloads until the reality of poor accuracy sank in and the idea of having to use more planes to get the same tonnage of bombs to the target crossed over to using fewer but slower aircraft to get the same tonnage.
The last B-17Gs went:
Weights: 32,720 pounds empty, 55,000 pounds normal loaded, 72,000 pounds maximum.

Make sure you are comparing like to like.

As far as the single tail B-24s goes, just look at the pictures.

640px-PB4Y-2_Privateer_VP-23_in_flight.jpg

85602_1526496100.jpg

This was converted to be an air tanker for firefighting. Not sure if the tail was changed or not. The engines are Wright R-2600s to help get the plane off the runway and to help pull outs at the end of a canyon.
You have an awful lot of tail and just like wings, a high aspect ratio tail (tall and skinny vs short and wide) will give a different bite on the air.
 
What about the "Liberty Lad" which participated on Operation Tidal Wave and came back with two engines lost on one side(!) after an 16 hours flight?
"...drop pretty much like a rock." sounds like a bit of an exaggeration.
Well that "exaggeration" was from a gentleman who flew multiple missions in the aircraft, was shot down and taken prisoner, so I think he might be just a tad biased! There were many aircraft that flew on Tidal Wave that made it back with extensive damage, it does show a side of the aircraft for being somewhat rugged, but at the same time this ill-planned mission showed some of the deficiencies with the aircraft. Hell, the lead aircraft spiraled into the sea for no apparent reason!

From Wiki -

The formation reached the Adriatic Sea without further incident; however aircraft #28, Wongo Wongo, belonging to the 376th Bombardment Group (the lead group, about 40 B-24s)[​ and piloted by Lt. Brian Flavelle began to fly erratically before plunging into the sea due to unknown causes
 
Look again at the B-17 weights provided. The B-17 could have gained nearly 10 tons between the E and G but even if the G was taking off at 65,000lbs and had trouble on the way in or while forming up it was in a very deferent flight regime than when coming back.
Some of the accounts of both B-17s and B-24s coming back with 2 engines not running involve judgment calls on when they started throwing out the ammo and other items of equipment. Once they were pretty sure they were out of the range of enemy aircraft ALL of the ammo went out the side and a fair number of .50 cal guns went to, subject to how much effort and/or tools needed. There were also judgment calls on how hard to push the remaining engines (how long since last overhaul?) as well as battle damage. Did you have two engines konk out or did they help from AA guns or a few hundred machine gun bullets? Or to put it another way, different bombers had different amounts of open space exposed to the slipstream that weren't there on take off in not actual large flaps of sheet metal acting like air brakes.
In some cases they had controls shot up and the damaged air craft had to fly an even more crablike course than a plane that had all functioning control surfaces and could trimmed to a better degree. You loose both engines on one side you may run out of trim authority ;)
 
Some of the accounts of both B-17s and B-24s coming back with 2 engines not running involve judgment calls on when they started throwing out the ammo and other items of equipment. Once they were pretty sure they were out of the range of enemy aircraft ALL of the ammo went out the side and a fair number of .50 cal guns went to, subject to how much effort and/or tools needed. There were also judgment calls on how hard to push the remaining engines (how long since last overhaul?) as well as battle damage. Did you have two engines konk out or did they help from AA guns or a few hundred machine gun bullets? Or to put it another way, different bombers had different amounts of open space exposed to the slipstream that weren't there on take off in not actual large flaps of sheet metal acting like air brakes.
In some cases they had controls shot up and the damaged air craft had to fly an even more crablike course than a plane that had all functioning control surfaces and could trimmed to a better degree. You loose both engines on one side you may run out of trim authority ;)
Great point! Well documented, even in movies. When limping home the crew jettisoned everything they possibly can.
 
I would guess on two engines they were trying to get down to the 32,000-33,000lb empty weight plus crew weight and enough fuel to land?
I would think the goal would be to keep it aloft until safe, then decide on landing or bailing out. Of concern with two out on one side is also fuel balance. Cross feeding (fuel management) would be required to keep the wings close to the same weight. Having two dead on one side causes the wing to be heavy (requires more rudder / aileron displacement which in turn causes more drag). I would think there were quite a few decisions to land due to wounded not being able or safe to bail out (opine).

Cheers,
Biff
 
I would guess on two engines they were trying to get down to the 32,000-33,000lb empty weight plus crew weight and enough fuel to land?
From that piece I posted earlier...

After Harry's twelfth mission, the original crew Harry trained with was assembled and assigned a combat mission. Their assigned primary target for this mission was the rail yards at Vienna, Austria with the secondary target being the Messerschmitt factory at Regensburg, Germany.

By this time, Harry had completed far more missions than any other members of his original crew. The date of this final mission was March 26, 1945. The crew was able to complete the bombing run over Vienna, but upon turn out and setting a course back to the base, they encountered flak and lost the number three engine. On the B-24, the number three engine provides hydraulic pressure for the landing gear and landing flaps in addition to other flight systems.

Since the B-24 cannot maintain altitude with only three operational engines, Harry's plane had to drop out of the bomber formation making it a prime target for German fighters and flack. Fortunately, as they began to fall behind and lose altitude, a Red-Tailed P-51 joined up with the stricken bomber and provided protection from the German fighter planes.

With only three engines operational, the B-24 bomber was losing altitude at about one hundred feet per minute. As the navigator, Harry was expected to calculate how far the plane could fly given the altitude loss and fuel remaining. Based on his calculations, Harry figured the plane would be able to reach an alternate runway under so called "friendly" control. The crew "dumped' everything out of the airplane at this time to try and maintain altitude for as long as possible.

Since the B-24 did not fly well on three engines, the pilot was required to push up the remaining three engines to their maximum operational limits. After two hundred miles of flying on only three engines, the number one engine coughed and shut down, leaving only two engines remaining. The B-24 bomber began to rapidly lose altitude.

The pilot announced that the plane could not make it to a safe landing site and they would have to attempt a crash landing. He also informed the crew that they could bailout as B-24 crash landings were not often very successful. The entire crew decided to stay with the airplane and hoped to survive a cash landing.

The pilot selected a farmer's pasture for the attempted landing site. As the plane came down, the crew were directed to manually crank down the landing gear since there was no longer hydraulic pressure available with the loss of the number three engine. During the excitement, the crew forgot to crank down the nose landing gear, which meant only the two main landing gears were down and locked at landing.

They crashed near Zagreb, Yugoslavia which was located about 250 miles behind German lines at the time. Fortunately, the field they landed in was very soft and grass covered. It was filled with cows, and luckily for the crew, no cows were harmed during the crash or the farmer might have taken some deadly action toward the crew as civilians were prone to do during this time of war. The escorting Red-Tailed P-51 made several passes over the downed airplane and departed with a wag of his wings saying good-by to the crew. Harry credits that P-51 pilot for saving the B-24 and enabling the crew to land without further harm.

During the crash, the tail of the plane actually rose up and the nose of the plane dug a deep trench in the soft earth. This was a result of the nose landing gear not being down and most likely prevented the plane from breaking apart and killing most of the crew. The crew was shaken up, but no one sustained any serious injuries.


 
Why did the single tail work better?
I thought a twin tail is suited to be more in the airstream of the engine blade (2 engines and more) and thus provide more control.
Maybe someone can explain it from aerodynamical view.

All I can do is cite from The B-24 Liberator: A Pictorial History by Allan G. Blue:
Consolidated recognized at an early date that a single tail configuration for the Liberator might prove highly desirable, but because of the press of early production commitments it was not until 10 October 1942 that the first wind tunnel tests got under way on a model incorporating this feature. When they gave encouraging results, B-24D 42-40058 was selected as a test article. Known as the B-24ST (for Single Tail) . . . [t]his version continued the flight test programme until June when, on the 29th of that month, the entire rear fuselage assembly of 42-40058 was removed and spliced to another similarly-dissected Liberator, B-24D-40-CO 42-40234 . . . [n]ow with its grafted on single fin empennage, 42-40234 was given the designation XB-24K . . .

After a series of flights from San Diego, the first of which took place on 9 September 1943, the XB-24K was flown to the USAAF Proving Ground Command at Elgin Field for official tests. Elgin's experienced B-24 pilots—not usually given to superlatives in their reports—found it decidedly superior to any other B-24 they had flown. Handling characteristics and manoeuverability were excellent, controls more sensitive, directional stability increased, and performance with two engines out on the same side was a great improvement over the standard B-24. Also noted were large increases in the fields of fire of the top turret, ball turret, tail turret and waist guns. Without qualification, Elgin recommended on 26 April 1944 that 'an empennage of similar design be incorporated in all future production B-24 aircraft' and preliminary contract negotiations were initiated for an unprecedented order of 4,500 B-24K machines. In time this resulted in the B-24N.

— p.59
 
Regarding the B-24's performance and characteristics:

During World War II, complaints from the operational theatres concerning lack of aircraft performance could often be traced to the fact that the aircraft was being operated under conditions far in excess of design specifications. Yet when changes were made to improve lagging performance, the theatres invariably used these improvements to further increase maximum loads instead of taking the improvement in terms of the increased performance that was originally requested.

Under this axiom, the B-24J was as a routine being flown on missions at gross weights in excess of 36 tons and flying characteristics suffered accordingly. Liberator controls had always been heavy, and continual addition of weight made them worse. It was extremely difficult to fly a tight formation with the B-24J, and so tiring that many pilots found it physically impossible after a few hours. The slow rate of roll, an inborn characteristic of the Liberator because of the large wing span, had been made slower by the addition of the outer wing tanks. Initial climb of a combat-loaded B-24 was slow, usually taking about six minutes to reach the 1,000 ft mark. Visibility from the flight deck was inadequate for formation flying. Because of the manner in which the side windows sloped inward, the pilot and co-pilot had be be seated low in order to have enough head room. This made it difficult to see over the instrument panel. In addition, the astrodome and the top of the nose turret were directly in front of the windshield which, to begin with, was considered too narrow and already partly blocked by the above-the-dash location of the compass. Furthermore, the side windows were so small that it was dangerous for the pilot to put his head through the window while taxiing. Lack of visibility from the nose compartment was equally serious—the only way the bombardier could adequately see was to get down on his hands and knees, and it was impossible for the navigator to help in target identification because of the lack of window area.

The Eighth Air Force experimented with various means of reducing the weight and visibility problems of the Liberator, including the removal of all ball turrets in July 1944 and the addition of various additional window areas in the nose. General Doolittle eventually rejected the Liberator on the grounds of too much weight and too little visibility and it was his intention, if sufficient B-17's could be obtained, to convert the entire Eighth Air Force to the Fortress.

The B-24 Liberator: A Pictorial History by Allan G. Blue, pp. 61 and 63
 
I recall an account of an Eighth Air Force B-17 crewman who joked that on mixed group missions, the B-24 was the best escort a B-17 could have - because they flew lower and looser and so the German fighters and flak preferred to attack them.

German fighter pilots thought something similar too. There are multiple accounts stating the B-24s were a preferential target and had a tendency to catch fire, explode or suffer wing failure when hit. The B-17 was seen as more resilient, requiring more accurate shooting if in a rear quarter attack. Head on attacks were considered to have about the same success rate for either aircraft.
 
When landed wheels up the B-24 fuselage often broke into three sections. This happened more often landing in water. There is a video elsewhere on the forum of a test landing on the Potomac? river.
 

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