The wing of the Learjet Model 60 was tailored for improved aerodynamic characteristics using the TRANAIR transonic full-potential computational fluid dynamics (CFD) code. A root leading edge glove and wing tip fairing were shaped to reduce shock strength, improve cruise drag and extend the buffet limit. The aerodynamic design was validated by wind tunnel test and flight test data.


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    Titel :

    Aerodynamic tailoring of the Learjet Model 60 wing



    Kongress:

    SAE, Aerotech ''93 ; 1993 ; Costa Mesa, CA, United States


    Erscheinungsdatum :

    01.01.1993



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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