Overall configuration requirements which represent view of group conducting research at NASA Langley Research Center; problem areas of takeoff noise, sonic boom, airframe and engine life; examination of cruise performance, stability, materials and structures, aeroelastic considerations, and engine configurations; advances in performance capability and operational flexibility can be achieved through incorporation of variable wing sweep and advanced fan type engine. (see also abstract in SAE -- J v 69 n 7 July 1961 p 32-6)


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    Title :

    Supersonic transport -- Required characteristics of configurations


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1961 Supersonic



    Publication date :

    1961


    Size :

    12 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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