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Impact of an exhaust throat on semi-idealized rotating detonation engine performance
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Authors:
Paxson, Daniel E.
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NASA Glenn Research Center
Year: 2016 Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center,
Year: 2016 Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center,
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Abstract
Keywords
Computational fluid dynamics. --- Exhaust flow simulation. --- Fuel flow. --- Inviscid flow. --- Propulsion system performance.
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