Luminescence-Based Surface Measurement Technique for Simultaneous Pressure and Temperature Measurements within Non-Oxygen Based Hypersonic Ground Test Facilities
Summary
The Department of War Air Force AFMC seeks proposals to develop and validate a luminescence‑based surface measurement technique that can simultaneously measure pressure and temperature in non‑oxygen hypersonic wind tunnels. This capability would replace limited discrete methods and enable global data collection for advanced hypersonic testing facilities.