Dynamics of three-dimensional shock-wave/boundary-layer interactions
DV Gaitonde, MC Adler - Annual Review of Fluid Mechanics, 2023 - annualreviews.org
Advances in measuring and understanding separated, nominally two-dimensional (2D)
shock-wave/turbulent-boundary-layer interactions (STBLI) have triggered recent campaigns …
shock-wave/turbulent-boundary-layer interactions (STBLI) have triggered recent campaigns …
Optical fiber Bragg grating-based measurement of fluid-structure interaction on a cantilever panel in high-speed flow
Optical fiber Bragg grating (FBG) technology offers many advantages over conventional
electrical sensors for the measurement of fluid-structure interaction (FSI). In this work, FBGs …
electrical sensors for the measurement of fluid-structure interaction (FSI). In this work, FBGs …
Aeroelastic experiments and companion computations assessing the impact of impinging shock sweep
KR Brouwer, R Perez, TJ Beberniss… - AIAA Scitech 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0945. vid Wind-tunnel experiments
were conducted to investigate the effects of swept impinging shock/boundary layer …
were conducted to investigate the effects of swept impinging shock/boundary layer …
Surface pressure measurements and predictions in shock-dominated flows
KR Brouwer, R Perez, TJ Beberniss… - AIAA Aviation 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-4134. vid Experiments on a rigid
panel were conducted to characterize the mean and unsteady pressure fields beneath a …
panel were conducted to characterize the mean and unsteady pressure fields beneath a …
Numerical Study of Hypersonic Fluid-Structure Interaction on a Cantilevered Plate With Shock Impingement Using Low and High Fidelity Numerical Methods
This research presents a numerical study of the University of New South Wales Canberra's
Hypersonic Multibody Aeroelastic eXperiment (HyMAX) using both low-fidelity modeling …
Hypersonic Multibody Aeroelastic eXperiment (HyMAX) using both low-fidelity modeling …
Effects of Aerothermal Shape Distortion on Hypersonic Vehicle Performance in Cruise
This paper explores the effects of aerothermal shape distortion upon the aerodynamic
performance of a hypersonic vehicle. A reference waverider vehicle was designed to …
performance of a hypersonic vehicle. A reference waverider vehicle was designed to …
Design of Aerothermoelastic Experiments in the AFRL Mach 6 High Reynolds Number Facility
ZB Riley, R Perez, KR Brouwer - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0948. vid An experiment was
recently conducted in the Air Force Research Laboratory Mach 6 High Reynolds Number …
recently conducted in the Air Force Research Laboratory Mach 6 High Reynolds Number …
Design of a wind tunnel model to investigate hypersonic double-swept shock boundary layer interaction
A preliminary computational hypersonic model of a double-swept shock generator impinging
on a panel structure within Mach 5.8 flow equivalent to that of the TUSQ hypersonic tunnel …
on a panel structure within Mach 5.8 flow equivalent to that of the TUSQ hypersonic tunnel …
Hypersonic Aerothermal Computations of a Sharp Fin Interaction
JM Signorelli, IR Higgins, SA Maszkiewicz… - … FORUM AND ASCEND …, 2024 - arc.aiaa.org
Substantial research has been completed towards understanding and simulating
shock/boundary-layer interactions, but efforts have only recently begun to understand the …
shock/boundary-layer interactions, but efforts have only recently begun to understand the …
Measuring fluid structure interaction in a cantilevered panel using optical fiber Bragg Gratings
View Video Presentation: https://doi. org/10.2514/6.2023-3605. vid This work explores the
use of optical fiber Bragg gratings (FBGs) to measure the Fluid Structural Interaction (FSI) on …
use of optical fiber Bragg gratings (FBGs) to measure the Fluid Structural Interaction (FSI) on …