Ion doping apparatus and method for aerodynamic flow control

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 21/00 (2006.01) B64C 23/00 (2006.01)

Patent

CA 2345260

Method and apparatus for impingement on the sonic wave produced by a supersonic gas flow and the gas flow in a boundary layer of a gas that interfaces with a solid substrate comprising providing a source of a mixture of ions and electrons, introducing said ions and electrons into the region behind the sonic wave and ahead of the boundary layer, separating said ions and said electrons in said region maintaining a substantial portion of said ions proximate said region and maintaining a substantial portion of said electrons remote from said region.

L'invention concerne un procédé et un dispositif d'impact sur l'onde acoustique produite par un flux gazeux et par un flux gazeux supersonique dans une couche limite d'un gaz faisant interface avec un substrat solide. Le procédé selon l'invention comporte les étapes suivantes: apport d'une source d'un mélange d'ions et d'électrons; introduction desdits ions et électrons dans la zone au-delà de l'onde acoustique et en decà de la couche limite; séparation desdits ions et électrons dans ladite zone en conservant une partie substantielle des ions à proximité immédiate de ladite zone et une partie substantielle des électrons éloignée de ladite zone.

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