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30 января 2011 г.
University of Washington Seattle Air Force Institute of Technology Wright-Patterson Air Force Base, Ohio Design and development of Aarcraft propulsion systems, Turbopropulsion combustion technology, Engine/Airframe performance matching, Inlets and inlet/engine integration, Variable convergent-divergent exhaust nozzle aerodynamics, Engine operability, Aeroelasticity and unsteady aerodynamics.