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:
Category Archives: News
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.

Panel methods for aircraft aeroelasticity
The review paper by G. Dimitriadis on panel methods for subsonic aircraft aeroelasticity is now available online: A review of fast unsteady aerodynamic and aeroelastic calculation methods for subsonic aircraft design.

AIAA SciTech 2026 Forum and Exposition
In January 2026 Greg Dimitriadis attended the AIAA SciTech Forum and Exposition, SciTech 2026, held in Orlando, Florida. We presented a paper entitled A Novel Surrogate-Assisted Structural Optimization Framework for Full-Aircraft Configurations.
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.

3AF International Conference Keynote
In March 2025 Greg Dimitriadis presented one of the keynote lectures at the 59th 3AF International Conference AERO 2025 in Starsbourg. The title of the lecture was ‘Fast unsteady aerodynamic and flutter calculations for subsonic and transonic aircraft’.
SDPMflut version 0.6 relese
New year, new version. You can download version 0.6 of the SDPMflut software here. New functionalities and two new test cases.

Von Karman Institute Lecture Course on Aeroelasticity
G. Dimitriadis will participate in the teaching of the AELAST course Introduction to Aeroelasticity: Aircraft and Turbomachinery at the Von Karman Institute for Fluid Dynamics, March 3-7 2025.

AIAA SciTech 2025 Forum and Exposition
In January 2025 we attended the AIAA SciTech Forum and Exposition, SciTech 2025, held in Orlando, Florida. We presented a paper entitled An unsteady supersonic Mach panel method.
Transonic Corrections for the Unsteady Compressible Source and Doublet Panel Method
Our paper on how to correct the predictions of the unsteady compressible Source and Doublet Panel Method for transonic effects is now available online:
