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...
محفوظ في:
| المؤلف الرئيسي: | |
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| التنسيق: | أطروحة |
| اللغة: | English |
| منشور في: |
Kuala Lumpur :
Kulliyyah of Engineering, International Islamic University Malaysia,
2017
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| الموضوعات: | |
| الوصول للمادة أونلاين: | Click here to view 1st 24 pages of the thesis. Members can view fulltext at the specified PCs in the library. |
| الوسوم: |
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