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Tichenor, Nathan R. (2010-10). Characterization of the Influence of a Favorable Pressure Gradient on the Basic Structure of a Mach 5.0 High Reynolds Number Supersonic Turbulent Boundary Layer. Doctoral Dissertation.
Thesis
Characterization of the Influence of a Favorable Pressure Gradient on the Basic Structure of a Mach 5.0 High Reynolds Number Supersonic Turbulent Boundary Layer
Overview
Overview
ETD Chair
Bowersox, Rodney
Ford I Professor and Head
publication date
October 2010