Numerical data and implementation for transient aeroelasticity of telescoping–folding morphing wings using a geometric pressure-port Birkhoffian framework

They cover pressure-work and kinematic checks, Goland and three-segment flutter calculations, conservative formulation comparisons, actuator-limited responses, and dynamic, continuous-frozen and frozen-library comparisons. A separate benchmark archive contains operation counts and the original balanced timing observations.

The pressure test uses a manufactured field; literature reference values are anchors, not measurements performed by the authors. The timing results apply to the recorded algorithms and hardware. No experimental or flight-test dataset is claimed.