It is shown that large portion of drag of long range subsonic aircraft is viscous and subject to performance improvement by laminarization; to achieve this, portion of boundary layer must be sucked from affected wing surface and pumped overboard; principle of laminar flow aircraft; means of obtaining power to drive suction compressor are classified and comparison of performance of 3 classes of propulsion systems shown; tabulation of performance and weights of turbojets and turbofans.


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    Titel :

    Propulsion systems for laminar flow aircraft


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Connors, J.W. (Autor:in) / Pfenninger, W. (Autor:in) / Smith, C.B. (Autor:in)

    Erschienen in:

    Aerospace Engineering ; 20 , n 8 ; p 16-17 + 70-79


    Erscheinungsdatum :

    1961


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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