International Forum on Aeroelasticity and Structural Dynamics

In June 2026 we participated in the International Forum on Aeroelasticity and Structural Dynamics IFASD 2026, held in Göttingen, Germany. Together with our collaborators, we presented five papers:

  • Aeroelastic stability calculations of a laminar wing using viscous-inviscid interaction, A. Crovato, C. Liauzun, P. Dechamps, G. Dimitriadis and V. Terrapon, IFASD-2026-0124
  • Limit Cycle Oscillation predictions using the Harmonic Balance Method and the nonlinear Source and Doublet Panel Method, G. Dimitriadis and V. Laraspata, L. Soria, IFASD-2026-0167
  • Aerostructural analysis and optimization using viscous-inviscid interaction, P. Dechamps, A. Crovato, G. Dimitriadis and V. Terrapon, IFASD-2026-0242
  • SDPMflut: an open-source unsteady Source and Doublet Panel method for flutter analysis, G. Dimitriadis, IFASD-2026-0148
  • Aircraft-level aeroelastic optimization using global-local structural modelling, S. Kilimtzidis, D. Zamani, A. Panani, G. Dimitriadis, V. Kostopoulos, S. Psarras, IFASD-2026-0205
  • SDPMflut version 0.8 release

    The latest version of SDPMflut has just been released. You can download version 0.8 of the SDPMflut software here. Among other improvements, the software now includes the ability to model fuselages. Several new test cases have been added.

    Wing-fuselage combination with wake
    Wing-fuselage combination with wake

    SDPMflut version 0.72 release

    New version for the holidays. You can download version 0.72 of the SDPMflut software here. The software now includes aerodynamic calculations and flutter analysis by means of both the Source and Doublet Panel Method and the nonplanar Doublet Lattice Method. One new test case has been added.