Date of Award

2010

Document Type

Thesis

Abstract

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.

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