碩士 / 國立成功大學 / 航空太空工程學系 / 88 / This thesis presents a winged-airship design by attaching an additional wing onto the conventional airship to enhance airship flight stability and operational capability by lift and control via wing surfaces. Based on this concept, by aerodynamic parameter estimation, the static characteristics for this winged airship is evaluated. The dynamic stability for the winged-airship is approximated from aircraft motion equations by linear perturbation process to include all aerodynamic parameters to solve the dynamic characteristics in horizontal situation. Following this model structure and process, the design practice studies a feasible wing profile to obtain the best wind resistance and control performance. The result of aerodynamics analysis and dynamics simulation of the winged-airship this study offers an important basis to support the continuous studies on flight navigation and control.
| Identifer | oai:union.ndltd.org:TW/088NCKU0295081 |
| Date | January 2000 |
| Creators | Kuo-Ming Lee, 李國銘 |
| Contributors | Chin E Lin, 林清一 |
| Source Sets | National Digital Library of Theses and Dissertations in Taiwan |
| Language | zh-TW |
| Detected Language | English |
| Type | 學位論文 ; thesis |
| Format | 85 |
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