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Gordon C. Oates Aircraft Propulsion Systems Technology and Design
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.
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