The provisions of this project call for the design of the structure of the wing and carry-through structure for the Viper primary trainer, which is to be certified as a utility category trainer under FAR part 23. The specific items to be designed in this statement of work were Front Spar, Rear Spar, Aileron Structure, Wing Skin, and Fuselage Carry-through Structure. In the design of these parts, provisions for the fuel system, electrical system, and control routing were required. Also, the total weight of the entire wing planform could not exceed 216 lbs. Since this aircraft is to be used as a primary trainer, and the SOW requires a useful life of 107 cycles, it was decided that all of the principle stresses in the structural members would be kept below 10 ksi. The only drawback to this approach is a weight penalty.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aircraft Wing Structure Detail Design


    Beteiligte:
    G. L. Sager (Autor:in) / R. Roberts (Autor:in) / B. Mallon (Autor:in) / M. Alameri (Autor:in) / B. Steinbach (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    36 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aircraft wing structure detail design

    Sager, Garrett L. / Roberts, Ron / Mallon, Bob et al. | NTRS | 1993


    Aircraft Wing Structural Detail Design (Wing, Aileron, Flaps, and Subsystems)

    R. Downs / M. Zable / J. Hughes et al. | NTIS | 1993


    Aircraft wing structural detail design (wing, aileron, flaps, and subsystems)

    Downs, Robert / Zable, Mike / Hughes, James et al. | NTRS | 1993



    Aircraft empennage structural detail design

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