
Subsonic Viscoelastic Deformation Measurement Protocol for Aircraft Thermoplastic Panels
Optical digital image correlation paired with laser vibrometry measures transient viscoelastic creep and aeroelastic damping in subsonic aircraft panels.

Optical digital image correlation paired with laser vibrometry measures transient viscoelastic creep and aeroelastic damping in subsonic aircraft panels.

Accommodate thermoplastic thermal expansion using kinematic sliding mounts and recessed lap joints to prevent out-of-plane buckling and boundary layer tripping.

Aerodynamic baseline testing for thermoplastic skins demands decoupled thermal load separation, unyielding boundary layer control, and high bandwidth pressure mapping.

Coupled aerodynamic pressure and thermal expansion amplify polymer skin deflection by up to 42%, requiring ground-based multi-environmental wind tunnel testing to prevent structural failure.
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