Batchelor Prize Lecture: Measurements in wall-bounded turbulence

AJ Smits - Journal of Fluid Mechanics, 2022 - cambridge.org
Our understanding of turbulent boundary layer scaling and structure has advanced greatly in
the past 20 to 30 years. On the computational side, direct numerical simulations and large …

Measurement of hypersonic turbulent boundary layer on a flat plate using cylindrical focused laser differential interferometer

R Huang, W Liu, J Cheng, J Wu - Physics of Fluids, 2023 - pubs.aip.org
ABSTRACT A modified Cylindrical-Focused Laser Differential Interferometer (CFLDI) system
was used to measure the density fluctuations generated by a Mach 6 turbulent boundary …

Thermal response of a nanoscale hot-wire in subsonic and supersonic flows

F Brunier-Coulin, DC Barros, A Piqué, M Hultmark… - Experiments in …, 2023 - Springer
A comprehensive characterization of the thermal response of nanoscale hot-wire probes is
performed in both subsonic and supersonic flows. A constant current anemometer was …

Comparison of hot-wire and particle image velocimetry measurements in the zone of interaction of a shock wave with a boundary layer at Mach number of 1.43

OI Vishnyakov, PA Polivanov, AA Sidorenko - Physics of Fluids, 2021 - pubs.aip.org
The interaction of a shock wave with a laminar boundary layer was studied at the low
supersonic Mach number M= 1.43. The measurements were carried out by particle image …

Micro-anémométrie pour l'aérodynamique: développement et application à la mesure de la turbulence aérothermique

B Baradel - 2023 - hal.science
La turbulence est un phénomène important présent dans de nombreux écoulements, qu'ils
soient naturels ou à application industrielle, et qui se caractérise notamment par une grande …

Mach Number Independent Hot-Wire Anemometry

P Dupont - 2023 - apps.dtic.mil
A comprehensive characterization of the thermal response of nanoscale hot-wire probes is
performed in both subsonic and supersonic flows. A constant current anemometer was …