The sensors are used in many flow environments and from subsonic to hypersonic speeds. In the following some highlights are presented:

HYPERSONIC TRANSITION & SECOND-MODE INSTABILITY MODES

Experiments in the NASA Langley Aerothermodynamics Laboratory
20-Inch Mach 6 Tunnel studying transition on a flat plate boundary layer can be found here.

ROTATING DETONATION ENGINE MEASUREMENTS

First measurment results are presented at AIAA Scitech-Conference 2025: MHz Rate In-Situ Direct Surface Heat-Flux Measurements in a Rotating-Detonation Engine (AIAA-2025-2146)

MEASUREMENTS IN SMALL-CORE TURBINE OVER-TIP SHROUD

Results of unsteady heat flux measurements in the tip-shroud of a small-core squealer-tip blade turbine at Purdue Experimental Turbine Aerothermal Lab (PETAL) can be found here.

INTERNAL COMBUSTION ENGINES: FORMULA SPORTS ENGINE

Experiments in the formula sports engine test rig of Siegfried Spiess Motorenbau GmbH, Germany studying the local heat-transfer in a combustion chamber can be found here.