| Title: | Design considerations of stopped-rotor cyclopter for mission to Venus |
| Authors: | Sema Husseyin, Author |
| Material Type: | ISU internship report |
| Publisher: | Illkirch-Graffenstaden (France) : International Space University, 2016 |
| Size: | 1 electronic resource (45 p.) / col. ill. |
| Bibliography note: | Includes bibliographical references |
| Languages: | English |
| Subjects: | Unmanned aerial vehicle |
| Description: | My project considers the use of a cycloidal blade system as a means of providing lift and propulsive thrust as well as combined with a stopped rotor system, to create a stopped-rotor cyclocopter vehicle for use during a mission to Venus. This stopped-rotor cyclocopter will be capable of flying at all atmospheric levels of Venus as well as land on the surface for scientific investigation. Three reference conceptual designs with different stopped-rotor cyclocopter yaw angles are tested in RotCFD as well as a model of a hovering cyclorotor for comparison with past work in the literature and innovative study for future projects. |
| ISU program : | Master of Space Studies |
| Permalink: | https://isulibrary.isunet.edu/index.php?lvl=notice_display&id=9881 |
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 Husseyin, Sema_INT report (3.68MB) Adobe Acrobat PDF |
