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


    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
    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

    PublisherTech Science Press


    ConferenceIntern. Conference on Computational & Experimental Engineering & Sciences


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

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