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    Aeroelastic modeling of the active flexible wing wind-tunnel model (1991)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The primary issues involved in the generation of linear, state-space equations of motion of a flexible wind tunnel model, the Active Flexible Wing (AFW), are discussed. The codes that were used and their inherent assumptions and limitations are also briefly discussed. The application of the CAP-TSD code to the AFW for determination of the model's transonic flutter boundary is included as well.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 2; p 497-53
    Format: application/pdf
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