Reference is made to projected Anglo-French supersonic airliner which is designed to cruise at Mach 2.2 (1450 mph); it has been concluded that basic aluminum structure is feasible at Mach numbers as high as 2.2; new problems raised by increasing Mach numbers are deterioration of material, effect of thermal stresses, and need for more elaborate and sophisticated procedures for full-scale proofing tests of air-frame; engines, systems difficulties, and noise problems are also discussed.


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    Titel :

    Problems facing supersonic transports


    Weitere Titelangaben:

    Engineering


    Erschienen in:

    Engineering ; 194 , n 5030


    Erscheinungsdatum :

    1962


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Supersonic Transports

    Online Contents | 1994


    Powerplants for supersonic transports

    Rapp, G.C. | Engineering Index Backfile | 1958


    Powerplants for supersonic transports

    Rapp, G.C. | Engineering Index Backfile | 1958


    Materials for supersonic transports

    RARING, R. | AIAA | 1964