a reply to:
ignorant_ape
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Here are some links which may explain some EXAMPLES
of HOW Plasma Sheathing may be used for reducing
aerodynamic friction on Ultra High Speed aircraft
which may use advanced engine technologies that
can ALSO cause Donuts-on-a-Rope during high-speed flight!
From what I understand about the use of
plasma sheathing, Space Shuttle-like
speeds (11,000 MPH or 17,000 KMH+ !!!)
in atmosphere can be achieved and if
one ALSO USES hull dimpling (i.e. put golf ball-like
dimples on the outer hull) a way to STABILIZE the
plasma sheath so that it "sticks better" to the
outer hull can further reduce aerodynamic drag.
See this link for a vehicle body example of hull dimpling:
www.autoblog.com...
In the case of high speed aircraft, the purpose of
dimpling is to create a rougher boundary layer of
highly disturbed and swirling plasma near each dimple
(i.e. 3D-XYZ volumetric plasma eddies) which lets
an OUTER sheath of superheated plasma push away
the atmosphere from the aircraft hull.
See laminar flow link:
en.wikipedia.org...
Each concave (or CONVEX!) dimple could be
from 1 cm up to 10 cm in diameter and have
an associated plasma ejection port which
is linked to a microwave cavity resonator
which uses MICROWAVES to heat the gas
being used as the basis of the plasma sheath.
See the following web Links which are part of
an amplification circuit which can super-heat a gas
such as helium, hydrogen, xenon, argon, neon, nitrogen, etc
to a plasma state to be injected just outside of
the outer hull to reduce aerodynamic drag.
Various Methods of Creating an Ionized Gas (i.e. Microwaves):
en.wikipedia.org...
Wikipedia Microwave Cavity Info:
en.wikipedia.org...
Microwave Cavity Resonator:
www.daenotes.com...
Commercially Sourced Plasma Generator:
www.sairem.com...
So here are some EXTRA web links which really show
HOW OLD some of this high speed aircraft plasma sheathing
research really is. Some of it is from as early as 1963 !!!!
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THIS IS THE "REALLY BIG DEAL" paper on this subject:
Aerodynamic Drag Reduction by Plasma and Hot-Gas Injection
by
Y. C. Ganiev; V. P. Gordeev; A. V. Krasilnikov;
V. I. Lagutin; V. N. Otmennikov; A. V. Panasenko
Journal of Thermophysics and Heat Transfer,
Vol. 14, No. 1 (2000), pp. 10-17. doi: 10.2514/2.6504
arc.aiaa.org...
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REALLY OLD PATENT ON PLASMA SHEATHING (Wing Surfaces?):
Patent # US3713157 A by North American Aviation Inc (1963)
www.google.ca...
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MODERN COMPUTER MODELLING OF SHEATHING FOR HIGH SPEED AIRCRAFT:
Finite Element Based Hydrodynamic Sheath Model
by Subrata Roy and B.P. Pandey
Computational Plasma Dynamics Laboratory
Kettering University Flint, MI 48504
cpdlt.mae.ufl.edu/roy/AIAA-02-2169.pdf
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Plasma Sheath Side-Issues:
Plasma Stealth for Aircraft:
en.wikipedia.org...
The Effect of a Plasma Sheath on Hypersonic Flight Communications by Hiroshi Taneda (1983)
dspace.mit.edu...
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As you can see some of this technology is from 1960's to the 1980's
to the Present Day and this means companies like Northrup, Boeing
and Lockheed Martin HIGHLY LIKELY are using such technologies
to build MACH 15+ Aircraft for high-altitude, high-speed
recon (i.e. SR-73 maybe?) or warfighting (FB-119 maybe?) purposes!
edit on 2015/2/11 by StargateSG7 because: sp