T. COLWILL, William T. Curran, Paul M Stiglic
Abstract
Integrated propulsion control system for ramjet Hypersonic Research Engine to operate at 3-8 Mach numbers
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Integrated propulsion control system for ramjet Hypersonic Research Engine to operate at 3-8 Mach numbers
Key concepts: Propulsion, Aeronautics, Aerospace engineering, Computer science, Control (management), Automotive engineering, Hypersonic speed, Engineering