Aerodynamic design and static stability of a hybrid buoyant aircraft /
Hybrid buoyant (HB) aircraft in which 50% of gross takeoff mass is supported by “free of cost aerostatic lift”, are a new arena to boost up the tourism and agricultural industry by leveraging on the new merger of lighter than air and heavier than air technologies. Due to non-availability of historic...
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| 主要作者: | |
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| 格式: | Thesis |
| 語言: | English |
| 出版: |
Kuala Lumpur :
Kulliyyah of Engineering, International Islamic University Malaysia,
2017
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| 主題: | |
| 在線閱讀: | Click here to view 1st 24 pages of the thesis. Members can view fulltext at the specified PCs in the library. |
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