I was just reading about Stealth technology when I come across article on wiki that it just kinda just clicked... well, let me rant on... 
The most interesting aspect of B2 is that it charges its leading edge to high electrical potential difference. This is a known fact, but most speculations points to towards "anti-gravity" or softening the sonic boom. I find that harder to believe, while the third possibility that it is for stealth, is the most likely answer.
From wiki : http://en.wikipedia.org/wiki/B-2_Spirit
For reasons not yet de-classified, the B-2 charges its leading edge to a very high electrical potential difference from its exhaust stream. It has been suggested (by Jane's Defence) that it augments the B-2's low thrust main engines. It is also a well known phenomenon that an ionised gas (plasma) will scatter a radar beam far more effectively than a solid surface of any conceivable shape. This could be the purpose of the high voltage leading edge.
From wiki : http://en.wikipedia.org/wiki/Plasma_stealth
"Plasma stealth is a proposed process that uses ionized gas to reduce the radar cross section (RCS) of an aircraft. Interactions between electromagnetic radiation and ionized gas have been extensively studied for a variety of purposes, including the possible concealment of aircraft from radar that plasma stealth theorizes. While it is theoretically possible to reduce an aircraft's RCS by wrapping the airframe in plasma, it may be very difficult to do so in practice. Various methods might plausibly be able to produce a layer or cloud of plasma around an airframe, from "simple" electrostatic or RF discharges to more exotic possibilities like laser produced plasmas."
Two points to reinforce my argument that this is true purpose of the high charge leading edge for stealth purpose, can be seen here :
1. The shorten length of bomber body. Why else would it be designed this way? The most obvious conclusion I can gather is that, the wing tip was charged to high electrical potentials to ionise the air that will flow around the body of the aircraft, thus creating a "plasma bubble". If you do the same with conventional aircraft design, it simply won't work because of the lengthen body - the plasma bubble is probably very hard to maintain the shape at the air traveling speed. This is probably the most logical reason for the B2 body to be designed this way, the length of the body is short, so that it is covered within the plasma bubble. Also, to increase the bomb load instead of lengthening the body (like a conventional bomber eg. B-52), the designers chosed to go horizontal to find space for bomb loads, reinforcing my speculation that the plasma bubble was the crux of the B2 stealth technology.
2. The extremely low top speed it can travel (Maximum speed: 410 knots (475 mph, 764 km/h). Perhaps, due to the technological limitation, that the B2 cannot sustain the "plasma shield bubble" at higher speed that the current specified without breaking the "bubble".
The most interesting aspect of B2 is that it charges its leading edge to high electrical potential difference. This is a known fact, but most speculations points to towards "anti-gravity" or softening the sonic boom. I find that harder to believe, while the third possibility that it is for stealth, is the most likely answer.
From wiki : http://en.wikipedia.org/wiki/B-2_Spirit
For reasons not yet de-classified, the B-2 charges its leading edge to a very high electrical potential difference from its exhaust stream. It has been suggested (by Jane's Defence) that it augments the B-2's low thrust main engines. It is also a well known phenomenon that an ionised gas (plasma) will scatter a radar beam far more effectively than a solid surface of any conceivable shape. This could be the purpose of the high voltage leading edge.
From wiki : http://en.wikipedia.org/wiki/Plasma_stealth
"Plasma stealth is a proposed process that uses ionized gas to reduce the radar cross section (RCS) of an aircraft. Interactions between electromagnetic radiation and ionized gas have been extensively studied for a variety of purposes, including the possible concealment of aircraft from radar that plasma stealth theorizes. While it is theoretically possible to reduce an aircraft's RCS by wrapping the airframe in plasma, it may be very difficult to do so in practice. Various methods might plausibly be able to produce a layer or cloud of plasma around an airframe, from "simple" electrostatic or RF discharges to more exotic possibilities like laser produced plasmas."
Two points to reinforce my argument that this is true purpose of the high charge leading edge for stealth purpose, can be seen here :
1. The shorten length of bomber body. Why else would it be designed this way? The most obvious conclusion I can gather is that, the wing tip was charged to high electrical potentials to ionise the air that will flow around the body of the aircraft, thus creating a "plasma bubble". If you do the same with conventional aircraft design, it simply won't work because of the lengthen body - the plasma bubble is probably very hard to maintain the shape at the air traveling speed. This is probably the most logical reason for the B2 body to be designed this way, the length of the body is short, so that it is covered within the plasma bubble. Also, to increase the bomb load instead of lengthening the body (like a conventional bomber eg. B-52), the designers chosed to go horizontal to find space for bomb loads, reinforcing my speculation that the plasma bubble was the crux of the B2 stealth technology.
2. The extremely low top speed it can travel (Maximum speed: 410 knots (475 mph, 764 km/h). Perhaps, due to the technological limitation, that the B2 cannot sustain the "plasma shield bubble" at higher speed that the current specified without breaking the "bubble".
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