Mitch Wolff, Ph.D. (Advisor); José A Camberos, Ph.D., P.E. (Committee Member); Mark A. Hagenmaier, Ph.D. (Committee Member)
Master of Science in Mechanical Engineering (MSME)
Shock wave-boundary layer interactions can significantly impact the operability of high-speed inlets by inducing flow separation. This flow separation is difficult to visualize in three-dimensional, inward-turning inlets because of the curved surfaces that form their internal flow paths. To remedy this challenge, a surrogate test article was created. Using the results from a previously completed Computational Fluid Dynamic (CFD) analysis of the HIFiRE-6, a surrogate inlet with a rectangular isolator section was streamline-traced, allowing for the use of schlieren imagery to capture the separation bubble. This thesis discusses the process of developing the test article. Experimental results from a planned future test entry will be compared to CFD results and wind tunnel results from previous tests, to examine the suitability of this surrogate.
Department or Program
Department of Mechanical and Materials Engineering
Year Degree Awarded
Copyright 2022, all rights reserved. My ETD will be available under the "Fair Use" terms of copyright law.