Improved aerothermodynamic instrumentation of an Allison T63-A-700 gas turbine engine
Approved for public release; distribution is unlimited. === This document describes the design, installation, and operation of an improved measurement system for the aerothermodynamic flow path states in an Allison T63-A-700 (C250-18 civilian designation). Temperature measurements for the gas genera...
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/5956 |