 | Hardest plane to take down in WW2?| Aviation Discuss Hardest plane to take down in WW2? in the World War II - Aviation forums; Originally Posted by Magister
The poser of the question knows best but I take it simply as a discussion as ... |
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02-01-2006, 03:30 PM
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#76 | | Senior Member
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Originally Posted by Magister The poser of the question knows best but I take it simply as a discussion as to wgich plane could absorbe more damage either by Japanese or German guns.
T-Bolt and Corsair both flew against the Japanese and only the T-Bolt flew against the Germans.
That doesn't mean we can't speculate! Hell, this board is all about speculation and that's the fun of it!
I'm sure the two aircraft are similar in being able to take damage but I come down on the T-Bolt side. (Maybe I'm biased)
All this talk of fabric and wood makes me want to build a tent.  | Oh I am not trying to kill people's fun, I just thought it was a legitamite question. I am in the Corsair camp and I am biased. So if I killed the discussion I am sorry.  But all of this stuff about fabric and wood makes me also want to make a big beduin tent.
I give you two camels for that Camel.
:{)
__________________ During World War II, Chuck Norris once shot down a German plane. He pointed his finger and yelled BANG! |
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02-01-2006, 03:31 PM
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#77 | | Banned
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Originally Posted by CurzonDax In this discussion I am on the Corsair camp. But the argument I have on this, and I might have missed it is that the Corsair never flew against the Luftwaffe where as the 'Bolt flew both against the Luftwaffe and the IJAF and IJN. I guess I don't really have an argument just an observation unless all are saying that a cannon shell is a cannon shell and that, and I am WAY ignorant on this, that Luftwaffe cannons had more hitting power, more muzzle velocity, and more explosive power than those of the Japanese. So if this be true, and again I am just trying to learn here, wouldn't this be a apples and oranges argument since the Corsair was never under Luftwaffe guns.
So therefore again if this is true, its not whether parts of the wings are fabric or not its what and whose cannon and for that matter machine gun, can do the most damage.
I hope I made sense.
:{) | The Japanese Type-II Mod 3 and beyond (used by the IJN) were comperable to the Hispano except the muzzle velocity was a bit lower at around 750 m/s. Its ~130 gram round certainly hit harder than the German 20mm, though of course it packed less HE. It had better ballistics than the Hispano round because them Japanese were crazy - they used unfused PETN rounds, which are so unstable they don't need a fuse. No fuse allowed the front of the round to be pointed. One has to wonder how many planes were lost when the gun blew up upon being fired?
They also used White Phosophorus incendiaries - everyone else considred WP too difficult and dangerous to handle to put it in small caliber aircraft cannon rounds. More than one US bomber thought it was going to make it home only to start decending and have the WP light up as the oxygen supply increased.
The Ho-5 (used by the IJA) was similar in hitting power to the Soviet ShVAK, but fired at 850+ rpm.
Japanese 20mm, after the Type II-mod 1 of the early Zero, were decently powerful cannon.
=S=
Lunatic |
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02-01-2006, 03:33 PM
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#78 | | Banned
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Originally Posted by FLYBOYJ Quote: |
Originally Posted by Lunatic Quote: |
Originally Posted by FLYBOYJ here's a list of synthetic fabics used on aircraft....
Dacron® Registered trade name for polyester fibres made by E.I. DuPont de Nemours & Company. Poly-Fiber® (and all it's other pseudonyms) is Dacron material.
Ceconite® Registered trade name for a fabric woven from polyester fibres and covering process. Application is with nitrate and butyrate dopes.
Stits Fabric Generic name for a fabric covering process developed by Mr. Ray Stits. Purchased by Poly-Fiber Inc in 1993 and renamed Stits Poly-Fiber.
Poly-Fiber®ii Registered trade name for a fabric woven from polyester fibre. A Poly-Fiber Inc material and process. Application is with Poly-Fiber® products.
Razorback® Registered trade name for a glass fibre fabric and covering process.
Superflite® Registered trade name for a fabric woven from polyester fibres and covering process.
Madapolam A bleached cotton fabric with a soft finish used in covering wooden surfaces. Complies with British Standard (BS) F114. | That's very nice but none of those fabrics are for a WWII Corsair. They are all for civilian aircraft and damage from gunfire is not a serious consideration. | The point is similar (earlier) materials were used during WW2.... | The point is you cannot compare civilian materials, optimized for weight cost effectiveness, and ease of use, with military materials optimized for combat useage. |
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02-01-2006, 05:43 PM
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#79 | | IP/Mech THE GREAT GAZOO
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Originally Posted by Lunatic Quote: |
Originally Posted by FLYBOYJ Quote: |
Originally Posted by Lunatic Quote: |
Originally Posted by FLYBOYJ here's a list of synthetic fabics used on aircraft....
Dacron® Registered trade name for polyester fibres made by E.I. DuPont de Nemours & Company. Poly-Fiber® (and all it's other pseudonyms) is Dacron material.
Ceconite® Registered trade name for a fabric woven from polyester fibres and covering process. Application is with nitrate and butyrate dopes.
Stits Fabric Generic name for a fabric covering process developed by Mr. Ray Stits. Purchased by Poly-Fiber Inc in 1993 and renamed Stits Poly-Fiber.
Poly-Fiber®ii Registered trade name for a fabric woven from polyester fibre. A Poly-Fiber Inc material and process. Application is with Poly-Fiber® products.
Razorback® Registered trade name for a glass fibre fabric and covering process.
Superflite® Registered trade name for a fabric woven from polyester fibres and covering process.
Madapolam A bleached cotton fabric with a soft finish used in covering wooden surfaces. Complies with British Standard (BS) F114. | That's very nice but none of those fabrics are for a WWII Corsair. They are all for civilian aircraft and damage from gunfire is not a serious consideration. | The point is similar (earlier) materials were used during WW2.... | The point is you cannot compare civilian materials, optimized for weight cost effectiveness, and ease of use, with military materials optimized for combat useage. | They're the same thing!!!! Grade A cotton is Grade A cotton - Ceconite is Ceconite - all the same spec....
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02-01-2006, 06:46 PM
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#80 | | Senior Member
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Originally Posted by Magister IMHO, the P-47 appears more structurally sound. | How can you base this on an observation? You dont know the thickness of each structural componant nor how they interact with adjacent components.
"more" does not necessarily = "increasing strength"
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02-01-2006, 07:04 PM
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#81 | | Senior Member
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| IMHO is just that ... an opinion. I have personally seen the fuselage skin thickness of both the Corsair and T-Bolt though and the T-Bolt is thicker. Lastly and as I indicated, I am biased.
Oh, and I am against fabric and wood too which is why I don't wera a skirt and a wooden leg. There wasn't just some fabric covering control surfaces either. "The entire wing ouside the fold behind the mainspar (about the rear 75%) was covered in fabric." (Lunatic) Also there were the areas made of wood. Don't even get me started on that. Bullets /cannon rounds striking wood does far more damage than strikes on aluminum.
In the end though, they were both pretty tough birds and I am left with my nagging bias.
__________________ MAGISTER |
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02-01-2006, 07:15 PM
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#82 | | Banned
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| Actually properly laminated wood holds up better against machine gun fire than aluminum. The down side is it is also heavier than metal.
Look to the La5-FN, La7, and Yak3 vs. Yak9 for info on this. The wood usually held up better than aluminum. Delayed action cannon rounds often did not detonate upon hitting wood. The only problem with the Soviet wood planes was the glue they used was flamable.
Now a solid piece of wood will shatter, that is true. But a laminated piece of wood can hold up quite well, retaining functionality even if a large hole is punched in it. |
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02-01-2006, 07:18 PM
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#83 | | IP/Mech THE GREAT GAZOO
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Originally Posted by syscom3 Quote: |
Originally Posted by Magister IMHO, the P-47 appears more structurally sound. | How can you base this on an observation? You dont know the thickness of each structural componant nor how they interact with adjacent components.
"more" does not necessarily = "increasing strength" | Great point! Look at the way both aircraft are built, you could almost see areas where engineers put emphasis on certain loads. The P-47 actually had a box structure within its wing, a technique still in use...
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02-01-2006, 07:23 PM
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#84 | | IP/Mech THE GREAT GAZOO
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Originally Posted by Lunatic Actually properly laminated wood holds up better against machine gun fire than aluminum. The down side is it is also heavier than metal. | That depends on the type of aluminum structure. If you're talking skins, maybe, if you're talking main structures, wing attach points which are usually 7075 aluminum or even steel, no way....
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02-01-2006, 07:43 PM
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#85 | | Senior Member
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| That's crap Lunatic. Plywood, hardwood, "properly laminated wood", etc. does not fare better when hit by bullets and cannon rounds and you know better. Go out to a gun range and do a little experimentation. We'll have to chalk this one up to your inexperience.
The same projectile going through a "properly laminated wood" (as opposed to improperly laminated wood ???) structure vs. an aluminum one will do far more damage to the wooden one. And an explosive device will do far more damage to wood than aluminum.
While the cotton panty fabric on the Corsair's wings (there's my bias again) will not initiate the fuse on a HE round, a wooden structural piece definitely will. Wood is harder than you think. If a half inch piece of "properly laminated wood" will deform a bullet, it will damn sure set the fuse on an HE round.
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02-02-2006, 01:22 AM
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#86 | | Banned
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Originally Posted by FLYBOYJ Quote: |
Originally Posted by syscom3 Quote: |
Originally Posted by Magister IMHO, the P-47 appears more structurally sound. | How can you base this on an observation? You dont know the thickness of each structural componant nor how they interact with adjacent components.
"more" does not necessarily = "increasing strength" | Great point! Look at the way both aircraft are built, you could almost see areas where engineers put emphasis on certain loads. The P-47 actually had a box structure within its wing, a technique still in use... | So does the Corsair. In fact, the Corsair design is refered to as a "box within box" structure. This why, except for carrier landings, the Corsair was completely flight worthy even if the wing spars were removed. I believe the techinque originated with the DC3 (or DC2). |
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02-02-2006, 01:32 AM
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#87 | | Banned
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Originally Posted by Magister That's crap Lunatic. Plywood, hardwood, "properly laminated wood", etc. does not fare better when hit by bullets and cannon rounds and you know better. Go out to a gun range and do a little experimentation. We'll have to chalk this one up to your inexperience.
The same projectile going through a "properly laminated wood" (as opposed to improperly laminated wood ???) structure vs. an aluminum one will do far more damage to the wooden one. And an explosive device will do far more damage to wood than aluminum.
While the cotton panty fabric on the Corsair's wings (there's my bias again) will not initiate the fuse on a HE round, a wooden structural piece definitely will. Wood is harder than you think. If a half inch piece of "properly laminated wood" will deform a bullet, it will damn sure set the fuse on an HE round. | Look into the Soviet experiance with their "greywood" and birch aircraft. A bullet puches a nice round hole in it, where metal often deforms. Soviet wooden aircraft were quite durable given their weight class. Look at the Mosquito, which also was a relatively durable aircraft.
The thing is, the best wood for such construction is not "hard".
You should also maybe look at how the fuses worked. Many fuses had to hit something sufficiently hard to trigger them. If the were deformed slowly (comparatively) they often did not trigger.
Besides, the thing I think you miss is that the metal aileron is typically like a small wing, composed of framing and ribbing covered with very thin sheet metal. The wooden ailerons of the Corsair were solid wood, much much thicker than the material of the metal aileron. What do you think is stronger, 3/4-2 inches of birch plywood or two thin sheets of dural stretched over dural framing approximately 1/32" thick? |
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02-02-2006, 02:10 AM
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#88 | | Senior Member
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| What do you think is stronger, 3/4-2 inches of birch plywood or two thin sheets of dural stretched over dural framing approximately 1/32" thick?
The wood will experience much bigger holes from AP or ball ammo and likewise will suffer greater damage from explosive 2cm and 3cm shells.
Lunatic, where do you get 1/32" (.03125) thick sheets? The P-47's control surfaces utilized 24-ST that was thicker than that. At present, I can only find the thickness of the skin on the dive recovery flaps which was 24-ST that was .188 thick. (No, that is not a typo.)
P-47 hit by an 88mm round.
Marine Major Norman O'Bryan looks through the four-foot hole torn in the wing of his Corsair by flak on his 99th mission. Some structural images
Lower half of fuselage
Upper half of fuselage
Tail cone
Assemply of upper and lower halfs
Wing section
Ailerons 
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02-02-2006, 08:33 AM
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#89 | | IP/Mech THE GREAT GAZOO
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Originally Posted by Lunatic . Look at the Mosquito, which also was a relatively durable aircraft.
The thing is, the best wood for such construction is not "hard". | The initial construction isn't that difficult, repairs are hard and if done slightly wrong can be devastating. Quote: |
Originally Posted by Lunatic What do you think is stronger, 3/4-2 inches of birch plywood or two thin sheets of dural stretched over dural framing approximately 1/32" thick? | Depending on how it's constructed - the Aluminum structure!!!
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02-02-2006, 09:18 AM
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#90 | | IP/Mech THE GREAT GAZOO
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Originally Posted by Magister Lunatic, where do you get 1/32" (.03125) thick sheets? The P-47's control surfaces utilized 24-ST that was thicker than that. At present, I can only find the thickness of the skin on the dive recovery flaps which was 24-ST that was .188 thick. (No, that is not a typo.) | 24T (2024 T3 or T6) sheet comes in the following standard thicknesses....
.025
.032
.040
.050
.063
.080
.090
.100
.125
.190
As far as I know this was the norm since WW2. Several skins I've seen on WW2 fighters may stack up several sheets...
Nice photos Magister
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