A hydrogen-cooled structure for a fixed-geometry, airframe-integrated scramjet is described. The thermal/structural problems, concepts, design features, and technological advances are applicable to a broad range of engines. Convectively cooled airframe structural concepts that have evolved from an extensive series of investigations, the technology developments that have led to these concepts, and the benefits that accrue from their use are discussed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Recent advances in convectively cooled engine and airframe structures for hypersonic flight


    Contributors:
    Kelly, H. N. (author) / Wieting, A. R. (author) / Shore, C. P. (author) / Nowak, R. J. (author)

    Conference:

    Congr. of the Intern. Council of the Aeron. Sci. ; 1978 ; Lisbon



    Publication date :

    1978-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Convectively cooled structures

    Wieting, A. R. / Thornton, E. A. | NTRS | 1979




    Actively Cooled Airframe Structures for High-speed Flight

    Robert J. Nowak / H. Neale Kelly | AIAA | 1977


    Actively cooled airframe structures for high-speed flight

    Nowak, R. / Kelly, H. | Tema Archive | 1976