activity
20132023
most citedSparsity-promoting dynamic mode decomposition

911 citations · 1.1k across the 7 of their papers we have counts for

collaborators

7 papers

physics.flu-dyn2023

Three-dimensional receptivity of hypersonic sharp and blunt cones to free-stream planar waves using hierarchical input-output analysis

David A. Cook, Joseph W. Nichols

Understanding the receptivity of hypersonic flows to free-stream disturbances is crucial for predicting laminar to turbulent boundary layer transition. Input-output analysis as a r…

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-dyn2018★ 6 cited

Input-output analysis of Mach 0.9 jet noise

Jinah Jeun, Joseph W. Nichols

We examine amplifying behavior of small perturbations about Reynolds-averaged Navier-Stokes solutions (RANS) of a subsonic turbulent jet using input-output (I/O) analys…

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…

physics.flu-dyn2013★ 911 cited

Sparsity-promoting dynamic mode decomposition

Mihailo R. Jovanović, Peter J. Schmid, Joseph W. Nichols

Dynamic mode decomposition (DMD) represents an effective means for capturing the essential features of numerically or experimentally generated flow fields. In order to achieve a de…