Fuel-vortex interactions for enhanced mixing in supersonic flow

An experimental investigation was conducted to compare the supersonic mixing performance between a novel aerodynamic ramp injector and a physical ramp injector. The aerodynamic ramp injector consisted of nine, flush-wall jets arranged to produce multiplicative fuel-vortex interactions for mixing enh...

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Bibliographic Details
Main Author: Fuller, Raymond Preston
Other Authors: Aerospace Engineering
Format: Others
Language:en
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/38092
http://scholar.lib.vt.edu/theses/available/etd-06062008-154721/