Future aircraft may be hydrogen fueled and fly at hypersonic speeds. The resulting environments will require new structural concepts to satisfy performance goals. Large representative structures will have to be flight tested prior to commitment to a costly vehicle fleet. To perform flight tests, a versatile, economical, high-speed research airplane is defined. Results of this study including experimental considerations for a hypersonic research airplane are reported.


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    Titel :

    Structural Concepts and Experimental Considerations for a Versatile High-Speed Research Airplane


    Beteiligte:
    L. R. Jackson (Autor:in) / F. S. Kirkham (Autor:in) / J. P. Weidner (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    90 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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