
Aerodynamic Wind Tunnel Calibration Standards for High Speed Skins
Aerodynamic skin calibration requires verifying transducer step height under 5 micrometers and freestream noise below 0.05 percent before flight data release.

Aerodynamic skin calibration requires verifying transducer step height under 5 micrometers and freestream noise below 0.05 percent before flight data release.

Verification of thermoplastic composite assemblies under high Mach shock boundary layer interactions requires fast-response heat flux sensors and high-enthalpy testing to prevent matrix deconsolidation.
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