A successful brazing process was developed and evaluated for fabricating full-scale titanium-clad Borsic/aluminum skin-stringer panels. A panel design was developed consisting of a hybrid composite skin reinforced with capped honeycomb-core stringers. Six panels were fabricated for inclusion in the program which included laboratory testing of panels at ambient temperatures and 533 K (500 F) and flight service evaluation on the NASA Mach 3 YF-12 airplane. All panels tested met or exceeded stringent design requirements and no deleterious effects on panel properties were detected followng flight service evaluation on the YF-12 airplane.


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    Titel :

    Fabrication and Evaluation of Brazed Titanium-Clad Borsic/Aluminum Skin-Stringer Panels


    Beteiligte:
    T. T. Bales (Autor:in) / D. M. Royster (Autor:in) / R. R. Mcwithey (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    41 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Fabrication and evaluation of brazed titanium-clad borsic/aluminum skin-stringer panels

    Bales, T. T. / Royster, D. M. / Mcwithey, R. R. | NTRS | 1980


    Brazed Borsic/aluminum structural panels

    Bales, T. T. / Wiant, H. R. / Royster, D. M. | NTRS | 1977


    Brazed borsic/aluminum structural panels

    Bales, Thomas T. / Wiant, H. Ross / Royster, Dick M. | TIBKAT | 1977


    Brazed Borsic/Aluminum Structural Panels

    T. T. Bales / H. R. Wiant / D. M. Royster | NTIS | 1977