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Effect of Wall Temperature and Mach Number on the Turbulence Structure of Hypersonic Boundary Layers

Izaak Beekman, Stephan Priebe, Matthew Ringuette, Pino Martin
2009 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition   unpublished

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The characterization of the turbulence structure using statistical analysis 1 and a geometric packet-finding algorithm 2 is explored. We follow structures which have been identified by the geometric packet-finding algorithm, using automated object segmentation and feature tracking software, 3, 4 and observe how these structures and their associated wall signatures evolve in time. Using a direct numerical simulation database, we begin to assess the turbulence structure given by each method and the evolution of this structure.
doi:10.2514/6.2009-1328 fatcat:mfn4sg2k7bbqdp3epu4legajoi
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Izaak Beekman, Stephan Priebe, Matthew Ringuette, Pino Martin. "Effect of Wall Temperature and Mach Number on the Turbulence Structure of Hypersonic Boundary Layers." 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition (2009)