Sequential Multi-Disciplinary Optimization for the Conceptual Design of a Blended-Wing-Body Aircraft
Conference Paper
(2004)
Author(s)
G Carpentieri (TU Delft - System Engineering & Aircraft Design)
Michel Van Tooren (TU Delft - System Engineering & Aircraft Design)
G Bernardini (External organisation)
L Morino (External organisation)
Research Group
System Engineering & Aircraft Design
To reference this document use:
https://resolver.tudelft.nl/uuid:539dd0d3-243e-41ac-a44a-46db9dfe2785
More Info
expand_more
expand_more
Publication Year
2004
Research Group
System Engineering & Aircraft Design
Pages (from-to)
864-871
ISBN (print)
0-9657001-6-X
Abstract
The objective of the present work is the preliminary sizing of a BWB (Blended Wing Body) passenger aircraft configuration, using a multidisciplinary modelling and optimization methodology. The aim is to ensure that all the important aspects of the design are taken into account in a concurrent way.
No files available
Metadata only record. There are no files for this record.