1–11 von 11 Ergebnissen
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    The Design of Repairable Advanced Composite Structures

    Hart-Smith, L. J. | SAE Technical Papers | 1985

    Adhesive Bonding of Aircraft Primary Structures

    Hart-Smith, L. J. | SAE Technical Papers | 1980

    Interface Control-The Secret to Making DFMA® Succeed

    Hart-Smith, L. J. | SAE Technical Papers | 1997

    Lessons Learned from the DC-10 Carbon-Epoxy Rudder Program

    Hart-Smith, L. J. | SAE Technical Papers | 1986

    An Object Lesson in False Economies - The Consequences of Not Updating Repair Procedures for Older Adhesively Bonded Panels

    Hart-Smith, L. J. / Davis, M. J. / SAMPE | British Library Conference Proceedings | 1996

    The Curse of the Nylon Peel Ply

    Hart-Smith, L. J. / Redmond, G. / Davis, M. J. et al. | British Library Conference Proceedings | 1996

    Interface Control-The Secret to Making DFMA[R] Succeed

    Hart-Smith, L. J. / Society of Automotive Engineers | British Library Conference Proceedings | 1997

    Easily Assembled Structurally Efficient Joints in Metallic Aircraft Structures

    Hart-Smith, L. J. / International Committee on Aeronautical Fatigue | British Library Conference Proceedings | 1995
    Beteiligte: Grandage, J. M. , Jost, J. M.

    Making Fuselage Riveted Lap Splices with 200-Year Crack-Free Fatigue Lives

    Muller, R. P. G. / Hart-Smith, L. J. / International Committee on Aeronautical Fatigue | British Library Conference Proceedings | 1997

    Innovative Concepts for the Design and Manufacture of Secondary Composite Aircraft Structure

    Hart-Smith, L. J. / Institution of Engineers, Australia / Royal Aeronautical Society; Australian Division | British Library Conference Proceedings | 1993