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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Dynamic bumps for drag reduction at transonic-supersonic speeds

Invented by: Ahmed A. Hassan
Mesa, AZ

Bradley A. Osborne
Manchester, MO

Scott Schwimley
Foristell, MO

Garry Billman
Troy, MO

Mary Billman, legal representative
Troy, MO

Originally Assigned to: The Boeing Company
Chicago, IL
[Now assigned to . . .]

Issued:2011-09-13
Filed:2006-10-18
Application No:11583140
Examined by:Dinh; Tien

A system for reducing overall drag of a mobile platform includes a surface on which an airflow forms a boundary layer and a generally normal shockwave. The airflow is at a first velocity that is one of transonic and supersonic. An oscillating jet injects and extracts a jet flow through the surface. The jet flow is at a second velocity that is substantially less than the first velocity. A recirculation region is upstream of the normal shockwave and is disposed at least partially in the boundary layer. The recirculation region is established at least by the oscillating jet. A generally oblique wave is established by the recirculation region and weakens the normal shockwave to reduce the overall drag experienced by the surface.

[pdf] U.S. Pat. No. 8,016,245

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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