Sequential Multi-Disciplinary Optimization for the Conceptual Design of a Blended-Wing-Body Aircraft

G Carpentieri, MJL van Tooren, G Bernardini, L Morino

    Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

    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.
    Original languageUndefined/Unknown
    Title of host publicationAdvances in Computational & Experimental Engineering & Sciences
    EditorsA.J.B. Tadeu, S.N. Atluri
    Place of PublicationMadeira
    PublisherTech Science Press
    Pages864-871
    Number of pages8
    ISBN (Print)0-9657001-6-X
    Publication statusPublished - 2004
    EventIntern. Conference on Computational & Experimental Engineering & Sciences - Madeira
    Duration: 26 Jul 200429 Jul 2004

    Publication series

    Name
    PublisherTech Science Press

    Conference

    ConferenceIntern. Conference on Computational & Experimental Engineering & Sciences
    Period26/07/0429/07/04

    Keywords

    • conference contrib. refereed
    • Conf.proc. > 3 pag

    Cite this

    Carpentieri, G., van Tooren, MJL., Bernardini, G., & Morino, L. (2004). Sequential Multi-Disciplinary Optimization for the Conceptual Design of a Blended-Wing-Body Aircraft. In A. J. B. Tadeu, & S. N. Atluri (Eds.), Advances in Computational & Experimental Engineering & Sciences (pp. 864-871). Tech Science Press.