Conceptual design and optimization methodology for box wing aircraft
A conceptual design optimization methodology was developed for a medium range box wing aircraft. A baseline conventional cantilever wing aircraft designed for the same mis- sion and payload was also optimized alongside a baseline box wing aircraft. An empirical formula for the mass estimation of the...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en |
| Published: |
Cranfield University
2013
|
| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/7938 |