Date of Award
The objective of this study is to effectively model and independently analyze the three dimensional forebody, inlet, and isolator of a conceptual Four-Point-Star Morphing Ramjet-Scramjet Engine. The analysis was conducted using computational fluid dynamic (CFD) softwares, namely, the Air Vehicle Unstructured Solver (AVUS) and FLUENTTM.
Grant, Jamil D., "Validation Of The Forebody Design Of A Ramjet-Scramjet Propulsion System Using Computational Fluid Dynamics" (2010). Theses. 15.