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Electroaerodynamic drag reduction...
I've been reading up on this, and supposedly they've achieved drag reductions of up to 96% at supersonic speeds, but only about 10% at subsonic speeds. Still, a 10% reduction in drag is pretty good, especially at only 20 watts total power expended (at 38,500 volts), as I saw in one subsonic study.
My thinking is to inject a high voltage plasma out front of the vehicle, with the opposing electrode at the rear of the vehicle. That'd do two things... it'd force the stalled air further forward, essentially creating a low-pressure void into which the vehicle moves, and it'll help to reattach the air flow near the rear of the vehicle as the charged air seeks the opposite polarity electrode. That leaves a smaller wake, thus you get drag reduction. Has anyone tried this? |
Yeah, but all the flashing from bug zapping proved to be too great a distraction.
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Is it like the anti-gravity stuff on the B-2 bomber? |
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Brown.edu Research Projects (PDF) "The energy was deposited instantaneously along a finite length of the cone axis, ahead of the cone's bow shock, causing a cylindrical shockwave to push air outward from the line of deposition. The shockwave would sweep the air out from in front of the cone, leaving behind a low-density column/tube of air, through which the cone (vehicle) propagated with significantly reduced drag. The greatest drag reduction observed was 96% (100% drag reduction would result in the complete elimination of drag forces on the cone). The propulsive gain was consistently positive, meaning that the energy saved due to drag reduction was consistently greater than the amount of energy "invested" (i.e. deposited ahead of the vehicle). The highest ratio of energy-saved/energy-invested was approximately 6500% (a 65-fold "return" on the invested energy)." Here's another good one: Nonequilibrium Plasma Aerodynamics (PDF) "Promising applications of plasma systems to control flow involve management of laminar-to-turbulent transition in the boundary layer, the management of flow detachment or attachment to the surface, and the resultant management of lift and drag force of an airfoil. The authors [Mhitaryan et al, 1961, 1964] demonstrated up to 30% drag force decrease and 40% lift force increase for airfoil with 460 mm chord length (AoA = 8 degrees), thickness of 13% and flap length 30% (AoA = 43 degrees) of the chord in velocity range from 8.75 to 20.4 m/s." |
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more discussion at https://en.wikipedia.org/wiki/Biefel...93Brown_effect Quote:
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tried this
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Using conventional streamlining techniques,this 80% of drag can be eliminated on an automobile,leaving 7-12% surface friction drag. Ionizing this 7-12% might yield only a 3 1/2-6% loss due to air friction,yielding a 1 3/4-3% mpg increase using gross reasoning. 1950's ionizing research was abandoned owing to inefficiencies in ionizing power requirements.Sounds like they've made a breakthrough in electronics.:) |
If air is effectively incompressible then Viktor Shauberger's biological submarine could also work in air.
http://ecomodder.com/forum/member-fr...logicalsub.gif |
also in air
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I'd be looking at modern high-bypass turbofans. |
The engineering is rudimentary. Maybe he was dumb-ing it down for his times. His inspiration was realizing trout can keep station in a moving stream of water by gulping water through their gills. They flick their tail when they want to go somewhere.
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