activity
20172025
most citedReattachment streaks in hypersonic compression ramp flow: an input-output analysis

124 citations · 230 across the 5 of their papers we have counts for

collaborators

5 papers

physics.chem-ph2025

Modified Marrone-Treanor dissociation model: formulation and benchmarking for diatom/atom mixtures

Ross S. Chaudhry, Erik Torres, Thomas E. Schwartzentruber +1

We present a modified Marrone-Treanor model for dissociation with rate parameters derived exclusively from quasiclassical trajectory calculations on ab initio potential energy surf…

physics.flu-dyn2023

Linear Analysis of Boundary-Layer Instabilities on a Finned-Cone at Mach 6

Daniel B. Araya, Neal P. Bitter, Bradley M. Wheaton +8

Boundary-layer instabilities for a finned cone at Mach=6, [m], and zero incidence angle are examined using linear stability methods of varying fidelity…

physics.flu-dyn2019★ 21 cited

Transient growth analysis of oblique shock wave/boundary-layer interactions at Mach 5.92

Anubhav Dwivedi, Nathaniel Hildebrand, Joseph W. Nichols +2

We study physical mechanisms that trigger transient growth in a high-speed spatially-developing laminar boundary layer that interacts with an oblique shock wave. We utilize an appr…

physics.flu-dyn2018★ 124 cited

Reattachment streaks in hypersonic compression ramp flow: an input-output analysis

Anubhav Dwivedi, G. S. Sidharth, Joseph W. Nichols +2

We employ global input-output analysis to quantify amplification of exogenous disturbances in compressible boundary layer flows. Using the spatial structure of the dominant respons…

physics.flu-dyn2017★ 85 cited

Simulation and stability analysis of oblique shock wave/boundary layer interactions at Mach 5.92

Nathaniel Hildebrand, Anubhav Dwivedi, Joseph W. Nichols +2

We investigate flow instability created by an oblique shock wave impinging on a Mach 5.92 laminar boundary layer at a transitional Reynolds number. The adverse pressure gradient of…