The mechanisms of unsteadiness in nominally two-dimensional (2-D) shock/turbulent- boundary-layer interactions (STBLIs) cannot be directly extended to three-dimensional (3-D) …
MC Adler, DV Gaitonde - Theoretical and Computational Fluid Dynamics, 2022 - Springer
Shock/turbulent-boundary-layer interactions (STBLIs) are ubiquitous in high-speed flight and propulsion applications. Experimental and computational investigations of swept, three …
Shock-Wave/Boundary-Layer Interaction (SBLI) is ubiquitous in high-speed air vehicles. SBLI surface flowfield properties of crossing shocks induced by symmetric Double-Fins …
In this study, a variation of the stacked stereoscopic PIV technique is proposed to perform fully volumetric (3-dimensions, 3-components) measurements of average flow fields within a …
Y Zhao, Y Zhou, Y Zhao - AIP Advances, 2024 - pubs.aip.org
Three-dimensional shock/boundary layer interactions (SBLIs) in the hypersonic inlet generate the separation vortex, which affects the flow uniformity of the inlet and can even …
View Video Presentation: https://doi. org/10.2514/6.2023-3575. vid Shock-Wave/Boundary- Layer Interaction (SBLI) is inevitable on supersonic and hypersonic air vehicles leading to …
Recent experimental and computational investigations have provided a comprehensive phenomenological description of unsteadiness in nominally two-dimensional (2-D) …
This thesis was developed during my three-and-a-half years as a PhD student at the Institute of Aerodynamics and Gas Dynamics (IAG) at the University of Stuttgart. First of all, I would …