Project

Feasibility Study of Using Matrix-Stabilized Combustion Technologies to Enable Ultra-low Emission Combustion in Aviation Gas Turbines

Discipline Area: 
Combustion
Propulsion
Principal Investigator: 
Organization: 
Stanford University
Program: 
LEARN
Round: 
3
Phase: 
Phase I
Period of Performance: 
Mar 1 2015 to Feb 29 2016
Co-Investigators: 
Waldo Hinshaw
John Sullivan (Stanford University)
Rebecca Fahrig (Seimens)

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