Reductions in drag of well over 90% are demonstrated for Mach numbers of 2, 4, 6 and 8, when our method
is applied. The drag quickly returns to its original value, when the method is "turned off."
Two papers describing the technology can be downloaded by clicking below:
is applied. The drag quickly returns to its original value, when the method is "turned off."
Two papers describing the technology can be downloaded by clicking below:
- Fluid Dynamics Paper
- Plasma Dynamics Paper
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| Supersonic/Hypersonic Drag Reduction Results |
drag reduction of a conical body traveling at Mach 2.
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Click to enlarge
drag reduction of a conical body traveling at Mach 4.
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Click to enlarge
drag reduction of a conical body traveling at Mach 6.
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Click to enlarge
drag reduction of a conical body traveling at Mach 8.
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Click to enlarge