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| Content Provider | IEEE Xplore Digital Library |
|---|---|
| Author | Ishtiaq, S. Israr, A. |
| Copyright Year | 2013 |
| Description | Author affiliation: Dept. of Mech. Eng., Inst. of Space Technol., Islamabad, Pakistan (Israr, A.) || Dept. of Aeronaut. & Astronaut., Inst. of Space Technol., Islamabad, Pakistan (Ishtiaq, S.) |
| Abstract | This study presents one of the methodologies that can be adopted to design variable wing geometry and its functionality. With this concept the aircraft is able to perform optimally under a variety of flight conditions. The major aspects discussed include the basic geometry design of a double delta aircraft for initial sizing, the selection and importance of the correct airfoil for the selected geometry and lastly how to find the pivot point for the variable wing mechanism that produces least overlapping issues. In addition, 3D modeling tool in Pro Eng is used to verify the results of selected airfoil. The results indicate a better overall performance for both flight regimes of subsonic and supersonic. |
| Starting Page | 1 |
| Ending Page | 4 |
| File Size | 280242 |
| Page Count | 4 |
| File Format | |
| ISBN | 9781479909933 |
| DOI | 10.1109/ICASE.2013.6785549 |
| Language | English |
| Publisher | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Publisher Date | 2013-08-21 |
| Publisher Place | Pakistan |
| Access Restriction | Subscribed |
| Rights Holder | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subject Keyword | Geometry Design Variable Drag Sweep Aerodynamics Pivot Aircraft Aircraft propulsion Automotive components Assembly Airfoil |
| Content Type | Text |
| Resource Type | Article |
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