This paper presents innovative research on how virtual enterprise technology, on top of the existing massive distributed computing environments, supports distributed collaboration in industrial aeronautic design and analysis. An information system supporting multi-disciplinary analysis for transonic wing design is realised, making use of a Java-based enterprise information architecture. This system provides users as well as other systems easy and controlled access to distributed computing resources as being used in aircraft development programmes. Neither specific software infrastructure nor specific IT knowledge are required for its usage. A prototype of this system, based on the proposed architecture, is illustrated and some example results for wing design in a virtual enterprise setting are shown.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Distributed collaborative and multi-disciplinary design of civil aircraft wings


    Additional title:

    Verteiltes gemeinschaftliches und multidisziplinäres Design von Zivilflugzeugflügeln


    Contributors:


    Publication date :

    2006


    Size :

    10 Seiten, 3 Bilder, 15 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Multi-Disciplinary Design & Analysis of Conceptual Flexible Wings

    Abdo, M. / Kayfeke, F. / Pepin, F. et al. | British Library Conference Proceedings | 2001


    Multi-Disciplinary Design of Aircraft Fuselage Structures

    van Tooren, Michael / Krakers, Lars | AIAA | 2007


    Disciplinary Implications of a System Architecting Approach to Collaborative Aircraft Design

    Walther, Jan-N. / Ciampa, Pier D. / Nagel, Björn | Springer Verlag | 2022



    Collaborative optimization with disciplinary conceptual design

    Rawlings, Mark / Balling, Richard | AIAA | 1998