Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Multi-Objective Six Sigma Approach Applied to Robust Airfoil Design for Mars Airplane


    Contributors:

    Conference:

    48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; 2007 ; Honolulu , Hawaii



    Publication date :

    2007-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Multi-Objective Six Sigma Approach Applied to Robust Airfoil Design for Mars Airplane AIAA Paper 2007-1966 CD-ROM Number 8

    Shimoyama, K. / Oyama, A. / Fujii, K. | British Library Conference Proceedings | 2007


    Mars Airplane Airfoil Design with Application to ARES

    Smith, Stephen / Guynn, Mark / Streett, Craig et al. | AIAA | 2003



    Aerodynamic Design of Airfoil for Flying Wing Mars Airplane

    Harada, Takuya / Fujita, Koji / Oyama, Akira et al. | AIAA | 2018


    A Study on Airfoil Design for Future Mars Airplane

    Oyama, Akira / Fujii, Kozo | AIAA | 2006