The purpose of this project is to provide an empennage structural assembly that will withstand the operational loads defined in FAR Part 23, as well as those specified in the statement of work, i.e. snow, rain, humidity, tiedown forces, etc. The goal is to provide a simple yet durable lightweight structure that will transfer the aerodynamic forces produced by the tail surfaces through the most efficient load path to the airframe. The structure should be simple and cost-effective to manufacture and repair. All structures meet or exceed loading and fatigue criteria. The structure provides for necessary stiffness and ease of maintenance.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aircraft Empennage Structural Detail Design


    Beteiligte:
    D. Lesnewski (Autor:in) / R. M. Snow (Autor:in) / L. M. Combs (Autor:in) / D. Paufler (Autor:in) / G. Schnieder (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    56 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aircraft Empennage Structural Detail Design

    G. Meholic / R. Brown / M. Hall et al. | NTIS | 1993


    Aircraft empennage structural detail design

    Meholic, Greg / Brown, Rhonda / Hall, Melissa et al. | NTRS | 1993


    Aircraft empennage structural detail design

    Lesnewski, David / Snow, Russ M. / Combs, Lisa M. et al. | NTRS | 1993


    AIRCRAFT EMPENNAGE

    GARCIA NIETO CARLOS / PEREIRA MOSQUEIRA FERNANDO / VELEZ DE MENDIZABAL ALONSO IKER et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT EMPENNAGE

    LINARES VILLEGAS MARIO / GARCIA TORAN SILVIA | Europäisches Patentamt | 2025

    Freier Zugriff