An Integrated Aerodynamic-Ramp-Injector/ Plasma-Torch-Igniter for Supersonic Combustion Applications with Hydrocarbon Fuels

The first integrated, flush-wall, aero-ramp-fuel-injector/plasma-torch igniter and flame propagation system for supersonic combustion applications with hydrocarbon fuels was developed and tested. The main goal of this project was to develop a device which could be used to demonstrate that the corre...

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Bibliographic Details
Main Author: Jacobsen, Lance S
Other Authors: Aerospace and Ocean Engineering
Format: Others
Published: Virginia Tech 2014
Online Access:http://hdl.handle.net/10919/28858
http://scholar.lib.vt.edu/theses/available/etd-09032001-185111/