The interest toward Mars exploration has been considerably increasing due to also the successful deployment of the Perseverance rover and the continuous tests developed by SpaceX's launch vehicle, Starship. While the Mars 2020 mission is currently in progress, the first controlled flight on another planet have been proven in April 2021 with the vertical take-off and landing of the Ingenuity rotorcraft on Mars. In addition, the rotorcraft Dragonfly is expected to achieve the same endeavor in Titan, the largest moon of Saturn, by 2036. Continuous efforts have been oriented toward the development of new technologies and aircraft configurations to improve the performance of current proposed designs to achieve powered flight in different planetary bodies. This thesis work is a preliminary study to develop a comprehensive analysis over the generation of optimum airfoil geometries to achieve vertical flight in environments where low Reynolds numbers and Mach number equal to 0.2 and 0.5.
| Identifer | oai:union.ndltd.org:unt.edu/info:ark/67531/metadc1873834 |
| Date | 12 1900 |
| Creators | Saez, Aleandro G. |
| Contributors | Manzo, Maurizio (Aerospace and mechanical engineer), Sadat, Hamid, Wasikowski, Mark, Ciarcia, Marco |
| Publisher | University of North Texas |
| Source Sets | University of North Texas |
| Language | English |
| Detected Language | English |
| Type | Thesis or Dissertation |
| Format | xi, 73 pages : illustrations (chiefly color), Text |
| Rights | Public, Saez, Aleandro G., Copyright, Copyright is held by the author, unless otherwise noted. All rights Reserved. |
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