Abstract
The Flight Research Laboratory at Texas A&M University has proposed conducting both natural laminar flow and passive laminar flow control flight test experiments through NASA’s Environmentally Responsible Aviation program in partnership with the Dryden Flight Research Center and the Langley Research Center. The flight test program will further explore discrete roughness element technology and demonstrate its effectiveness at extending laminar flow beyond the natural transition location. Texas A&M has completed a wing glove design, designated TAMU-06-05, that will be installed on a Gulfstream III testbed aircraft. Detailed analysis on the wing glove design effectiveness is given, focusing on flowfield behavior and boundary-layer stability characteristics near the glove using fullaircraft CFD calculations.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
