Atomic Layer Thermopiles: Comprehensive static calibration, comparison and application in subsonic and supersonic flows
- UAS Landshut - Thermal and Fluid Mechanics Lab, Bavaria (Germany)
- Purdue University, West Lafayette, IN (United States)
Here, this paper compares the calibration of different heat flux sensors in radiation- and convection-based sub- and supersonic operation. First, four heat flux sensors based on different principles: ALTP (Transverse Seebeck Effect), HFM-8E (differential-layer device), coaxial Thermocouple and a TG-2000 (circular-foil gage) are calibrated in a laser-based radiation setup. In a second step, all heat flux sensors are compared with a slug-calorimeter within a subsonic convection-dominated facility based on stagnation-point measurements of an impinging hot air jet. The obtained results indicate that a sensitivity transfer between a radiative calibrated sensor used in a mainly convective environment is not always possible and can lead to significant, systematic errors. Calibration in a subsonic shear flow with thermocouple readings demonstrate small divergence from the manufacturer provided sensitivity. Finally, supersonic testing with high frequency shock-boundary layer interactions highlight the need for ALTP rather than the conventional use of thermocouple arrays to resolve the high frequency phenomena associated with shock boundary layer interactions.
- Research Organization:
- Purdue University, West Lafayette, IN (United States)
- Sponsoring Organization:
- German Federal Ministry of Economical Affairs and Energy; USDOE
- OSTI ID:
- 2424389
- Journal Information:
- International Journal of Thermal Sciences, Journal Name: International Journal of Thermal Sciences Vol. 183; ISSN 1290-0729
- Publisher:
- ElsevierCopyright Statement
- Country of Publication:
- United States
- Language:
- English
Similar Records
Measured lengths of supersonic hydrogen-air jet flames -- compared to subsonic flame lengths -- and analysis
Three-Dimensional Inviscid Flow About Supersonic Blunt Cones at Angle of Attack, III: Coupled Subsonic and Supersonic Programs for Inviscid Three-Dimensional Flow