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Paxson, Daniel E.
ID:
1386438
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Paxson, Daniel E.
Paxson Daniel E.
Paxson Daniel E
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A sectored-one-dimensional model for simulating combustion instabilities in premix combustors
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A simplified model for detonation based pressure-gain combustors
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An incidence loss model for wave rotors with axially aligned passages
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Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine
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Ejector enhanced pulsejet based pressure gain combustors
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Examination of wave speed in rotating detonation engines using simplified computational fluid dynamics
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Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines
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Impact of an exhaust throat on semi-idealized rotating detonation engine performance
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Numerical analysis of a rotating detonation engine in the relative reference frame
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Numerical assessment of four-port through-flow wave rotor cycles with passage height variation
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Performance impact of deflagration to detonation transition enhancing obstacles
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The influence of unsteadiness on the analysis of pressure gain combustion devices
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Using the NASA GRC sectored-one-dimensional combustor simulation
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Wave augmented diffusers for centrifugal compressors
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