Please use this identifier to cite or link to this item:
|Title:||Aircraft morphing wing concepts with radical geometry change|
|Authors:||Min, Z. |
|Keywords:||Aircraft morphing wing|
Reversible deployable structure
|Citation:||Min, Z.,Kien, V.K.,Richard, L.J.Y. (2010). Aircraft morphing wing concepts with radical geometry change. IES Journal Part A: Civil and Structural Engineering 3 (3) : 188-195. ScholarBank@NUS Repository. https://doi.org/10.1080/19373261003607972|
|Abstract:||Aircraft morphing schemes affect flying performance of aircrafts by dramatic change of aircraft body shapes. Such schemes eliminate the need for multiple, expensive, mission-specific aircraft. Morphing designs include rotating, sliding and inflating based on shape change mechanisms. The current trend in technology development shows that there is room to improve with regards to aircraft size, flying range and flight performance envelope. There should be a balance between shape change and the penalties in cost, complexity and weight. Final performance of the morphing aircraft depends heavily on how such a balance is achieved. © 2010 The Institution of Engineers, Singapore.|
|Source Title:||IES Journal Part A: Civil and Structural Engineering|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Nov 16, 2018
checked on Oct 6, 2018
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.