1. Semi-Analytical Modeling of Shock-wave/Boundary Layer Interaction Over Compression Ramps in Hypersonic Flow Open Access Author: Glenn, Ryan Title: Semi-Analytical Modeling of Shock-wave/Boundary Layer Interaction Over Compression Ramps in Hypersonic Flow Area of Honors: Aerospace Engineering Keywords: Computational Fluid DynamicsHypersonic Flow File: Download Ryan_Banks_Glenn__Thesis_.pdf Thesis Supervisors: Daning Huang, Thesis SupervisorKenneth Steven Brentner, Thesis Honors Advisor
