PARAMETER STUDY A · FIXED AoA = 12°

U Sweep

Seven transient CFD anchors from 50 to 200 km/h provide a controlled test bed for spatial compression, coherent/residual decomposition, spectral modes and autonomous reduced dynamics.

7 speeds4,480 snapshots96,000 cells4 model/dynamics tests
ENGINEERING QUESTION

Which representation is useful—not merely compact?

The U Sweep deliberately keeps geometry and angle of attack fixed so model behavior can be compared without changing the underlying physics configuration. Each method asks a different question of the same CFD data.

Raw POD

Can a direct global linear basis plus simple phase/speed interpolation provide a transparent, deployable baseline?

Phase + Residual POD

Does explicitly separating repeatable coherent motion from secondary residual dynamics improve structure or deployment?

SPOD

Does conditioning the decomposition on frequency reveal a much simpler coherent representation?

SINDy

Can POD coordinates form a closed autonomous dynamical state rather than relying on prescribed phase?

METHODS IN PARALLEL

Different outcomes are part of the result

CROSS-METHOD TAKEAWAY

The hard part is increasingly temporal/state structure—not only spatial compression

Spatial compression

POD works well

All tested approaches confirm that important field content can be represented in a reduced spatial basis, especially coherent velocity and surface quantities.

Coherent dynamics

Strong periodic family exists

Cl/Cd phase diagnostics and SPOD both identify a consistent dominant aerodynamic oscillation across the seven speeds.

Residual dynamics

Not just one extra harmonic

The phase-residual analysis shows structured 2–6 f0 content together with substantial broadband/irregular residual variance.

Autonomous dynamics

Closure matters

SINDy shows that a low-dimensional oscillator can be discovered, but higher fidelity requires choosing a state with sufficient closure and possibly memory/coupling.

NEXT PARAMETER LAYERS

Do not assume the same dynamics survive a harder operating space

← Back to NACA0012 project map