The High Speed Civil Transport (HSCT) will be exposed to elevated temperatures during Mach 2.4 supersonic flight. While not as extreme as those encountered in other high speed flight efforts (NASP, Shuttle), thermal effects will impact decisions in almost all areas of material selection and design. Accurate temperatures are required to evaluate materials, structural concepts, cooling requirements, etc. Analyses show the importance of structural configuration, use of fuel as a heat sink, and surface properties on structural temperatures. Capability to accurately determine convection and radiation boundary conditions is important for future HSCT design.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Temperature Issues for a Mach 2.4 High Speed Civil Transport


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Aerospace Technology Conference and Exposition ; 1994



    Erscheinungsdatum :

    01.10.1994




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Temperature Issues for a Mach 2.4 High Speed Civil Transport

    Johnson, B. D. / SAE | British Library Conference Proceedings | 1994


    Concept Development of a Mach 1.6 High-Speed Civil Transport

    E. W. Shields / J. W. Fenbert / L. P. Ozoroski et al. | NTIS | 1999


    Concept development of a Mach 4 high-speed civil transport

    Domack, Christopher S. / Dollyhigh, Samuel M. / Beissner, Fred L., Jr. et al. | NTRS | 1990


    Concept Development of a Mach 4 High-Speed Civil Transport

    C. S. Domack / S. M. Dollyhigh / F. L. Beissner et al. | NTIS | 1990


    Concept development of a Mach 3.0 high-speed civil transport

    Robins, A. Warner / Dollyhigh, Samuel M. / Beissner, Fred L., Jr. et al. | NTRS | 1988