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Old 10-25-2008, 05:24 PM   #1
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Twin boom question

Hello everyone,

I was wondering about this the other day- what are the structural/aerodynamic advantages and disadvantages of twin boom aircraft like the P-38, Fokker G.1, FW-189, etc.?
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Old 10-25-2008, 06:31 PM   #2
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Hello everyone,

I was wondering about this the other day- what are the structural/aerodynamic advantages and disadvantages of twin boom aircraft like the P-38, Fokker G.1, FW-189, etc.?
Can't think offhand of an advantage other than two engines when one lets go (maybe - the bromide about the purpose of the second fan is to carry you safely to the crash site) - and frequently you can not only carry a larger payload but have more room for fuel and also have the potential for more power/wt ratio for acceleration and climb. Armament packaging is more efficient

In general, the cons are -

It is difficult to reduce drag of a twin to anywhere close to a well designed single.

It is heavier

It is bigger and easier to see

It has a higher rolling intertia

It is more expensive

It is more complicated and requires longer training

With twin engines in nacelles you have 'three' fuselages to create parasite drag.

Fuel transfer typically is more complicated

These are not universal truths... but food for thought?
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Old 10-25-2008, 07:44 PM   #3
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you can load up the nose with some serious firepower, peace of mind having two engines
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Old 10-25-2008, 07:55 PM   #4
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I always wondered what the performance of the P-38 would have been if it had a conventional fuselage like the mossie.

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Last edited by comiso90; 10-25-2008 at 08:05 PM.
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Old 10-25-2008, 08:37 PM   #5
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Interesting concept Cosimo. The horizontal stabilizer looks a little too small for the rest of the plane.
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Old 10-25-2008, 08:42 PM   #6
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Interesting concept Cosimo. The horizontal stabilizer looks a little too small for the rest of the plane.
I spent 73 seconds on it... I wast designing a new aircraft,,, just a quick sketch..
copy and paste
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Old 10-25-2008, 11:20 PM   #7
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In the case of the P-38 the booms may have allowed more internal space than "normal" nacelles. This is significant as turbochargers were installed, and it allowed the radiators to be mounted farther back on the boom. It allowed the use of a larger and higher AR horizontal stabilizer than would normally be practical for a fuselage mounted tail.


A twin boom configuration is also important in cases other than twin-engine a/c. Such as in a pusher configuration with the engine mounted on the rear of the central pod. This provides space for a central (unsynchronised) mounted armament like a twin, but the smaller size of a single engine a/c.

Twin boom push-pull aircraft (Fokker D.XXIII) are also something to be noted, and generally easier to arrange than the configuraton used on the Do 335. (and is occasionally used on modern aircraft)


It's advantageous for jets as well, as in the case of the Vampire (Venom, Sea Vixen) this allows for an aircraft with short intake and exhaust which minimizes thrust loss. (particularly important to early jets with relatively low thrust engines) Although single boom designs like the Me P.1101 gave similar advantages.
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Old 10-25-2008, 11:34 PM   #8
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In the case of the P-38 the booms may have allowed more internal space than "normal" nacelles. This is significant as turbochargers were installed, and it allowed the radiators to be mounted farther back on the boom. It allowed the use of a larger and higher AR horizontal stabilizer than would normally be practical for a fuselage mounted tail.
kk is quite right. In the case of the P-38, half of the reason for going with the twin-boom configuration was so that there was a place to put the (fairly large) turbo-superchargers; a conventional nacelle would not have worked for the Allison V-1710 engines AND the turbo-superchargers, there simply would not have been enough room. It also incidentally provided a convenient place to house the main landing gear.
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Old 10-25-2008, 11:35 PM   #9
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Comiso, here are some drawings of other P-38 configurations:
it came up in this thread: http://www.ww2aircraft.net/forum/avi...-a-9076-2.html (Why not a jet driven P-38?)


Interestingly, it included the twing boom push-pull arrangement I mentioned earlier.
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Old 10-25-2008, 11:45 PM   #10
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Stich, I think it could have worked, but the nacelles would have had to be long to have space (and proper positioning) for the landing gear. (or switch to a taildragger) The radiator could have gone under the foreward part of the nacelle, like the one on the P-40's nose.

However, with the large nacelles (probably weighing almost as much as the previous booms) and the added weight of the fuselage, the aircraft would probably have been somewhat heavier.


The push-pull twin boom configuration is interesting as it eliminates the extra drag and rotational inertia (though the small booms will still add some) of outboard placed engines, and is significantly simpler than the Do 335's arrangement. (however, only a small armament would be able to be sone mounted, and -except for an engine cannon- would have to be synchronized)


And, Bill, most of what you discussed was common to all twin engined aircraft. I think the question was what was the advantages of the twin boom configuration compared to wing mounted nacelles with a central fuselage. (though, as I introduced, there are many other possibilities for the twin boom arrangement)

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Old 10-26-2008, 01:33 AM   #11
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In the G.1 the configuration was made like this because the rear observer/gunner got a good view to all side (even under) while still being very close to the pilot, which was preferred by Fokker.
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Old 10-26-2008, 07:39 AM   #12
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As a side note after listening to lectures on the P-38 glacier girl and Ruff Stuff another advantage was that with the weapons in the center they where easier to aim. Conventunal fighters with the engine in front are subject to more vibration in the nose making it harder to aim. There is very little if any vibration in the nose of a P-38 when it comes to aiming during battle.

Also with all your guns in central locations they pack a greater punch then say a mustang that has to offset there guns to a certain range or distance to bring all guns into play to hit the target at the same time.
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Old 10-26-2008, 07:43 AM   #13
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Also has advantages of range, don't forget!
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Old 10-26-2008, 08:00 AM   #14
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Micdrow,

I noted that already in post #7. The twin-boom (single engine) pusher also allowed this. (the push-pull obviously would not)

Of course, you could still mount nose (or wing root) guns on a/c with a tractor propeller on the nose, but they would have to be synchronized (except for an engine gun) which reduced RoF and excluded weapons not able to be synchronized. The size and number of weapons are also more limited given they all have to fit around the engine and compete for ammo space. (except for wing root guns)

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Old 10-26-2008, 10:08 AM   #15
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You are all talking about the advantages which are shared between all twin engined fighters. I think the question was why a twin boom construction. I believe in several cases this was because of the visibility for the gunner in the rear. Could the P38 configuration been chosen because of the tricycle gear?
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