Study of tensile properties to evaluate strength potential available in titanium alloys, precipitation hardening, and cold worked metastable austenitic stainless steels, and super alloys; unstable crack propagation resistance under static loading; stability under long time load and temperature; nonsteady load and temperature; it is possible to define alloys and assess important variables in design of Mach 3 aircraft. (see also abstract in SAE -- J v 69 n 7, 8 July 1961 p 32-6, Aug p 84-7)


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    Title :

    Considerations in selection of wing and fuselage sheet materials for trisonic transports


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1961



    Publication date :

    1961


    Size :

    19 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    CONSIDERATIONS IN SELECTION OF WING AND FUSELAGE SHEET MATERIALS FOR TRISONIC TRANSPORTS

    Brown, W. F., Jr. / Espey, G. B. / Jones, M. H. et al. | NTRS | 1962


    Considerations in Selection of Wing and Fuselage Sheet Materials for Trisonic Transports

    Espey, G. B. / Jones, M. H. / Brown, W. F. | SAE Technical Papers | 1962


    Preliminary design considerations for structure of trisonic transport

    Childers, M.G. | Engineering Index Backfile | 1960



    Trisonic aerodynamic loads study

    Dunn, B. G. | NTRS | 1965