| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8058515 | Aerospace Science and Technology | 2016 | 24 Pages |
Abstract
From the conceptual study, the simplified approach provides the basic properties of the morphing structure to retrofit the baseline aircraft, which highlights the feasibility of this novel concept although further study is still needed for its detailed design and analysis.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Chen Wang, Hamed Haddad Khodaparast, Michael I. Friswell,