Atomic Layer Thermopiles: Comprehensive static calibration, comparison and application in subsonic and supersonic flows

K Huber, T Rödiger, L Bhatnagar… - International Journal of …, 2023 - Elsevier
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 …

[HTML][HTML] Experimental aerothermal characterization of surface air-cooled oil coolers for turbofan engines

A Broatch, P Olmeda, J García-Tíscar… - International Journal of …, 2022 - Elsevier
Thermal management is a major challenge for new generation turbofan aero-engines. One
of the most promising heat exchangers are the so-called surface air-cooled oil coolers …

Development of a lifetime pressure sensitive paint procedure for high-pressure vane testing

PAN Aye-Addo, G Paniagua… - Journal of …, 2022 - asmedigitalcollection.asme.org
Optical measurements based on fast response pressure sensitive paint (PSP) provide
enhanced spatial resolution of the pressure field. This paper presents laser lifetime PSP at …

Experimental analysis of Reynolds effect on flow detachment and sudden flow release on a wall-mounted hump

J Saavedra, G Paniagua - Experimental Thermal and Fluid Science, 2021 - Elsevier
The boundary layer detachment limits compact power plants' operation at moderate
Reynolds number in adverse pressure conditions. Flow detachment is promoted by the lack …

Application of femtosecond laser electronic excitation tagging (FLEET) velocimetry in a bladeless turbine

JM Fisher, J Braun, TR Meyer… - … Science and Technology, 2020 - iopscience.iop.org
Shock waves appear in numerous high-speed propulsion applications, including intakes,
nozzles, and transonic and supersonic turbomachinery. The aerodynamic performance in …

A review of high-speed rotating HP turbine heat transfer and cooling studies over the last decade in the oxford turbine research facility

C Falsetti, PF Beard… - … Expo: Power for …, 2022 - asmedigitalcollection.asme.org
Over the last years, advanced experiments under engine-representative conditions have
been performed in the Oxford Turbine Research Facility (OTRF) to obtain high-quality aero …

[HTML][HTML] Aero-thermal numerical characterization of blunt fin-induced shock wave–boundary layer interaction and its control through leading-edge cooling injection

F Lozano, J Saavedra, G Paniagua - Physics of Fluids, 2022 - pubs.aip.org
This study represents a novel evaluation of active flow control to alleviate the aerothermal
penalties created by the blunt fin-induced shock wave–boundary layer interaction. The …

Response of separated boundary layers to steady and pulsated flow injection

HD Nowak… - Journal of …, 2023 - asmedigitalcollection.asme.org
A new class of power generation devices that experiences increased losses due to bulk flow
separation in segments of their expected in-flight regime is emerging. As such, active flow …

Short engine intakes: Design and trade-off aerodynamic recommendations

U Vyas, J Braun, V Andreoli, G Paniagua - Aerospace Science and …, 2023 - Elsevier
This work sets forth a design procedure for compact, highly diffusive engine intakes for high
subsonic speed applications. The aerodynamic tradeoffs between cruise and take-off flights …

Uncertainty in high-pressure stator performance measurement in an annular cascade at engine-representative Reynolds and Mach

L Bhatnagar, G Paniagua… - … for Gas Turbines …, 2022 - asmedigitalcollection.asme.org
The betterment of turbine performance plays a prime role in all future transportation and
energy production systems. Precise uncertainty quantification of experimental measurement …