Abstract: An airfoil tip vortex mitigation arrangement comprising one or more flow directors configured and positioned to re-direct freestream air over a low pressure surface of an airfoil in such a way as to displace and weaken a main tip vortex generated at a tip of the airfoil.
Type:
Grant
Filed:
December 13, 2011
Date of Patent:
February 20, 2018
Assignee:
Lockheed Martin Corroration
Inventors:
Neal D. Domel, Eric F. Charlton, Daniel N. Miller
Abstract: An airfoil tip vortex mitigation arrangement comprising one or more flow directors configured and positioned to re-direct freestream air over a low pressure surface of an airfoil in such a way as to displace and weaken a main tip vortex generated at a tip of the airfoil.
Type:
Application
Filed:
December 13, 2011
Publication date:
June 13, 2013
Applicant:
Lockheed Martin Corroration
Inventors:
Neal D. Domel, Eric F. Charlton, Daniel N. Miller