Comment on 'active flutter control using generalized unsteady13; aerodynamic theory'

Vepa, R (1979) Comment on 'active flutter control using generalized unsteady13; aerodynamic theory'. Journal of Guidance and Control, 2 . pp. 446-447.

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    Abstract

    Recently Edwards et al. published a method for active flutter control and finite state modeling of aeroelastic systems. While this method is extremely good for two-dimensional airfoils in incompressible and supersonic flow, it is not clear exactly how useful it is in subsonic flow and for three-dimensional lifting surfaces. In the latter case explicit solutions for the pressure and airloads in the complex frequency domain are not available, and the construction of these solutions numerically is not an easy matter. To understand this, one must view the contribution of Ref. 1 in perspective, without all the mathematical trimmings.

    Item Type: Journal Article
    Additional Information: Copyright for this article belongs to AIAA
    Uncontrolled Keywords: Aeroelasticity;Airfoil profiles;Flutter analysis; Incompressible flow;Supersonic flow;Vibration damping; Aircraft control;Aircraft models;Lifting bodies;Pressure effects;Structural stability
    Subjects: AERONAUTICS > Aeronautics (General)
    AERONAUTICS > Aircraft Stability and Control
    Division/Department: Structures Division
    Depositing User: Ms. Alphones Mary
    Date Deposited: 24 Feb 2010
    Last Modified: 24 May 2010 09:39
    URI: http://nal-ir.nal.res.in/id/eprint/942

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