An unsteady, 3D, implicit upwind Euler/Navier-Stokes algorithm is here used to compute the flutter characteristics of Wing 445.6, the AGARD standard aeroelastic configuration for dynamic response, with a view to the discrepancy between Euler characteristics and experimental data. Attention is given to effects of fluid viscosity, structural damping, and number of structural model nodes. The flutter characteristics of the wing are determined using these unsteady generalized aerodynamic forces in a traditional V-g analysis. The V-g analysis indicates that fluid viscosity has a significant effect on the supersonic flutter boundary for this wing.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Calculation of AGARD Wing 445.6 Flutter Using Navier-Stokes Aerodynamics


    Contributors:

    Conference:

    AIAA Applied Aerodynamics Conference ; 1993 ; Monterey, CA, United States



    Publication date :

    1993-08-09


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Calculation of AGARD Wing 445.6 Flutter Using Navier-Stokes Aerodynamics

    Lee-Rausch, E. / Batina, J. / AIAA | British Library Conference Proceedings | 1993


    Calculation of AGARD Wing 445.6 flutter using Navier-Stokes aerodynamics

    LEE-RAUSCH, ELIZABETH / BATINA, JOHN | AIAA | 1993


    Transonic Flutter Dips of the AGARD 445.6 Wing

    Bret Stanford / Kevin Jacobson | NTRS


    Transonic Flutter Dips of the AGARD 445.6 Wing

    B. Stanford / K. Jacobson | NTIS | 2022