A process is presented by which aeroelastic analysis is performed by using an advanced computational fluid dynamics (CFC) code coupled with an advanced computational structural dynamics (CSD) code. The process is demonstrated on an F/A-18 Stabilator using NASTD (an in-house McDonnel Douglas Aerospace East CFD code) coupled with NASTRAN. The process is also demonstrated on an aeroelastic research wing (ARW-2) using ENSAERO (an in-house NASA Ames Research Center CFD code) coupled with a finite element wing-box structure code. Good results have been obtained for the F/A-18 Stabilator while results for the ARW-2 supercritical wing are still being obtained.


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    Titel :

    Aeroelastic Analysis of Modern complex Wings


    Beteiligte:
    R. K. Kapania (Autor:in) / M. K. Bhardwaj (Autor:in) / E. Reichenbach (Autor:in) / G. P. Guruswamy (Autor:in)

    Erscheinungsdatum :

    1996


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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