Wing section flutter prediction using ‘k’ and ‘p-k’ method | MATLAB | Aerospace Engineering

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Hi, I am currently working on my dissertation about an aeroelastic analysis of a rectangular, high aspect ratio wing. I am stuck with the flutter section of this, I need to develop a program that solves the aeroelastic equations of a 2-degree-of-freedom and 3-degree-of-freedom for a wing section model using the ‘k’ method and ‘p-k’ method by obtaning the real and imaginary parts of the flutter determinant complex eigenvalue problem for a range of reduced frequencies ‘k’ A file describing the methods is attached. Thank you for your time.

Skills: MATLAB, Aerospace Engineering

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Project ID: #26896578