Transition scenario in hypersonic axisymmetrical compression ramp flow
Mathieu Lugrin, Samir Beneddine, Colin Leclercq, Eric Garnier and, Reynald Bur

TL;DR
This study uses high-fidelity simulations and spectral analysis to investigate the transition process in hypersonic axisymmetrical compression ramp flow, revealing the roles of linear and nonlinear mechanisms in flow transition.
Contribution
It introduces a combined approach of spectral POD and resolvent analysis to understand flow transition mechanisms in hypersonic compression ramp flows.
Findings
Linear amplification of oblique modes drives transition.
Nonlinear interactions create elongated streamwise structures.
Early nonlinear interactions are crucial for transition.
Abstract
A high-fidelity simulation of the shock/transitional boundary layer interaction caused by a 15-degrees axisymmetrical compression ramp is performed at a freestream Mach number of 5 and a transitional Reynolds number. The inlet of the computational domain is perturbed with a white noise in order to excite convective instabilities. Coherent structures are extracted using Spectral Proper Orthogonal Decomposition (SPOD), which gives a mathematically optimal decomposition of spatio-temporally correlated structures within the flow. The mean flow is used to perform a resolvent analysis in order to study non-normal linear amplification mechanisms. The comparison between the resolvent analysis and the SPOD results provides insight on both the linear and non-linear mechanisms at play in the flow. To carry out the analysis, the flow is separated into three main regions of interest: the attached…
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