Please use this identifier to cite or link to this item:
https://ptsldigital.ukm.my/jspui/handle/123456789/577619| Title: | Aerostatic and aerodynamic modules of a hybrid buoyant aircraft : an analytical approach |
| Authors: | Haque Anwar U (IIUM) Asrar Waqar (IIUM) Omar Ashraf A. (IIUM) Sulaeman Erwin (IIUM) Ali Mohamed J. S. (IIUM) |
| Keywords: | Aerostatic lift Aerodynamic lift Hybrid bouyant aircraft Drag polar |
| Issue Date: | 2015 |
| Description: | An analytical approach is essential for the estimation of the requirements of aerodynamic and aerostatic lift for a hybrid buoyant aircraft. Such aircraft have two different modules to balance the weight of aircraft; aerostatic module and aerodynamic module. Both these modules are to be treated separately for estimation of the mass budget of propulsion systems and required power. In the present work, existing relationships of aircraft and airship are reviewed for its further application for these modules. Limitations of such relationships are also discussed and they provide a starting point for better understanding of design methodology of such aircraft. |
| News Source: | IIUM Engineering Journal |
| ISSN: | 1511-788X |
| Volume: | 16 |
| Pages: | 9-17 |
| Call Number: | Siri TA1.I485 |
| Publisher: | International Islamic University Malaysia (IIUM) |
| URI: | https://ptsldigital.ukm.my/jspui/handle/123456789/577619 |
| Appears in Collections: | Journal Content Pages/ Kandungan Halaman Jurnal |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| ukmvital_78389+Source01+Source010.PDF | 113.97 kB | Adobe PDF |  View/Open |
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