| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 5473004 | Aerospace Science and Technology | 2017 | 13 Pages |
Abstract
It has been observed that the applicable cyclic loading spectra, as major input parameter of fatigue analysis, largely depend upon the natural frequencies, damping and the stiffness of the structure. The results and discussions of the whole exercise may be beneficial while carrying out aero-elastic tailoring of composite aircraft wing. This research work has also a positive contribution towards multidisciplinary structural design optimization of aerospace vehicles.
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Waqas Anwar, M. Zubair Khan, Asif Israr, Shahid Mehmood, Nazeer A. Anjum,