Recent advances in feature extraction techniques for high-speed flowfields

S Unnikrishnan - Progress in Aerospace Sciences, 2023 - Elsevier
Abstract Space–time scale-resolved diagnostic and computational campaigns routinely
produce high-fidelity multi-disciplinary truth-model quality datasets for complex …

Reynolds-number effects on the acoustic disturbance environment in a Mach 6 nozzle

N Hildebrand, MM Choudhari, L Duan - AIAA Journal, 2023 - arc.aiaa.org
To understand the impact of the Reynolds number on the disturbance field inside a high-
speed wind tunnel, we use direct numerical simulations to model turbulent boundary layers …

Direct numerical simulation of acoustic disturbances in a hypersonic two-dimensional nozzle configuration

N Hildebrand, MM Choudhari, CP Deegan, J Huang… - AIAA Journal, 2022 - arc.aiaa.org
Direct numerical simulations (DNS) are performed to study acoustic radiation in a quasi-two-
dimensional nozzle with two independent spatially evolving turbulent boundary layers with …

Interaction of a tunnel-like acoustic disturbance field with a blunt cone boundary layer at Mach 8

Y Liu, M Schuabb, L Duan, P Paredes… - AIAA Aviation 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3250. vid The existing
measurements of laminar-to-turbulent transition over circular cones in conventional (ie," …

Transducer resolution effect on pressure fluctuations beneath hypersonic turbulent boundary layers

J Huang, L Duan, KM Casper, RM Wagnild, NP Bitter - AIAA Journal, 2024 - arc.aiaa.org
The size of a pressure transducer is known to affect the accuracy of measurements of wall-
pressure fluctuations beneath a turbulent boundary layer because of spatial averaging over …

Assessment of turbulence models in a hypersonic cold-wall turbulent boundary layer

J Huang, JV Bretzke, L Duan - Fluids, 2019 - mdpi.com
In this study, the ability of standard one-or two-equation turbulence models to predict mean
and turbulence profiles, the Reynolds stress, and the turbulent heat flux in hypersonic cold …

Direct numerical simulation of turbulent pressure fluctuations over a cone at Mach 8

J Huang, L Duan, KM Casper, R Wagnild… - AIAA Scitech 2020 …, 2020 - arc.aiaa.org
Direct numerical simulations (DNS) were conducted to characterize the pressure fluctua-
tions under the turbulent portion of the boundary layer over a sharp 7 deg half-angle cone at …

Nonlinear nonmodal analysis of hypersonic flow over blunt cones

A Scholten, P Paredes, MM Choudhari, F Li… - AIAA Journal, 2024 - arc.aiaa.org
The linear amplification of modal disturbances that lead to boundary-layer transition in two-
dimensional/axisymmetric hypersonic configurations is strongly reduced by the presence of …

Unsteady pressure measurement in the presence of a cavity between the sensor and the flow

A Gorbushin, E Anokhina, E Stolyarov - Sensors and Actuators A: Physical, 2023 - Elsevier
This study focuses on the measurement of unsteady pressure in gas flows with various
particle admixtures using miniature piezoresistive sensors. A variant of the classical …

Effect of the Reynolds number on the freestream disturbance environment in a Mach 6 nozzle

NJ Hildebrand, MM Choudhari, L Duan - AIAA AVIATION 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3776. vid To understand the impact
of Reynolds number on the acoustic disturbance field inside a high-speed wind tunnel, we …