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.
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.
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.
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’.
New year, new version. You can download version 0.6 of the SDPMflut software here. New functionalities and two new test cases.
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.
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.
Our paper on how to correct the predictions of the unsteady compressible Source and Doublet Panel Method for transonic effects is now available online:
SDPMflut version 0.5 has just been released. You can read about it and download it here.
Our paper on how to perform flutter calculations with the unsteady compressible Source and Doublet Panel Method is now available online: