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 Dryden Flight Research Center and 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 University completed a wing-glove design, designated TAMU-06-05, that was to 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 full-aircraft computational-fluid-dynamics calculations.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: 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.