Date of Award
Summer 2013
Document Type
Thesis
Degree Name
Master of Science (MS)
Department
Mechanical & Aerospace Engineering
Program/Concentration
Aerospace Engineering
Committee Director
Colin P. Britcher
Committee Member
Robert L. Ash
Committee Member
Brett A. Newman
Call Number for Print
Special Collections; LD4331.E56 G735 2013
Abstract
The research reported here has examined the potential improvements in overall aircraft performance that can result from integrating skin friction reduction technology, such as riblets, early in the aircraft design cycle. This study has shown that riblets can improve the payload capacity, increase the range, and improve performance of transport aircraft. If recent advances in fabrication techniques make it possible to create aluminum wing surfaces with integral riblet geometries, the applications could be widespread and the gains significant.
Rights
In Copyright. URI: http://rightsstatements.org/vocab/InC/1.0/ This Item is protected by copyright and/or related rights. You are free to use this Item in any way that is permitted by the copyright and related rights legislation that applies to your use. For other uses you need to obtain permission from the rights-holder(s).
DOI
10.25777/stjz-6877
Recommended Citation
Gregory, John M..
"Design Advantages of Skin Friction Drag Reduction Using Riblets"
(2013). Master of Science (MS), Thesis, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/stjz-6877
https://digitalcommons.odu.edu/mae_etds/512