Objectives - Environmentally Responsible Aviation (ERA) Project - NASA and The Boeing Company collaboration on damage arresting composites - 10% airframe weight reduction can provide significant reduction in fuel burn and emissions - Incremental improvements to conventional “tube & wing” configuration insufficient to meet the goals - HWB configuration promises significantly improved aircraft performance - HWB requires pressurized composite airframe with nearly flat panels that transfers significant mechanical loads - Explore PRSEUS as the primary structural concept for HWB


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    Titel :

    Testing and Analysis of a Composite Non-cylindrical Aircraft Fuselage Structure, Part II: Severe Damage


    Beteiligte:
    Adam Przekop (Autor:in) / Dawn Jegley (Autor:in) / Marshall Rouse (Autor:in) / Andrew Lovejoy (Autor:in) / Hsi-Yung T Wu (Autor:in)

    Kongress:

    2016 AIAA SciTech Conference ; 2016 ; San Diego, CA, US


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure, Part II: Severe Damage

    Przekop, Adam / Jegley, Dawn C. / Lovejoy, Andrew E. et al. | AIAA | 2016


    Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure, Part II: Severe Damage (AIAA 2016-2177)

    Przekop, Adam / Jegley, Dawn C. / Lovejoy, Andrew E. et al. | British Library Conference Proceedings | 2016


    Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure

    Przekop, Adam / Jegley, Dawn C. / Lovejoy, Andrew E. et al. | NTRS | 2016


    Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure

    Przekop, Adam / Jegley, Dawn C. / Lovejoy, Andrew E. et al. | NTRS | 2016


    Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure

    A. Przekop / D. C. Jegley / A. E. Lovejoy et al. | NTIS | 2016