A Performance Study of a Super-cruise Engine with Isothermal Combustion inside the Turbine
Current thinking on the best propulsion system for a next-generation supersonic cruising (Mach 2 to Mach 4) aircraft is a mixed-flow turbofan engine with afterburner. This study investigates the performance increase of a turbofan engine through the use of isothermal combustion inside the high-pressu...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/30202 http://scholar.lib.vt.edu/theses/available/etd-12212004-091959/ |