In the realm of aerospace design and performance, there are few boundaries in the never-ending drive for increased performance. This thirst for ever-increased performance of aerospace equipment has driven the aerospace and defense industries into developing exotic, extremely high-performance composites that are pushing the envelope in terms of strength-to-weight ratios, durability, and several other key measurements. To meet this challenge of ever-increasing improvement, engineers and scientists at NASA-Langley Research Center (NASA-LaRC) have developed a high-temperature metal laminate based upon titanium, carbon fibers, and a thermoplastic resin. This composite, known as the Hybrid Titanium Composite Laminate, or HTCL, is the latest chapter in a significant, but relatively short, history of metal laminates.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hybrid Titanium Composite Laminates: A New Aerospace Material


    Beteiligte:
    Johnson, W. S. (Autor:in) / Cobb, Ted Q. (Autor:in) / Lowther, Sharon (Autor:in) / St.Clair, T. L. (Autor:in)

    Erscheinungsdatum :

    01.01.1998


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Bearing Strength Analysis of Hybrid Titanium Composite Laminates

    Hundley, Jacob M. / Yang, Jenn-Ming / Hahn, H. Thomas et al. | AIAA | 2008



    High temperature hybrid titanium composite laminates: An early analytical assessment

    Johnson, W.S. / Li, E. / Miller, J.L. | Tema Archiv | 1996


    Metal laminates for aerospace applications

    Verbruggen, M. | Tema Archiv | 1990


    Delamination Properties of Aerospace Composite Laminates Containing Thin Interlaminar Holes

    Kousourakis, A. | British Library Conference Proceedings | 2005