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1
A sectored-one-dimensional model for simulating combustion instabilities in premix combustors by Paxson, Daniel E.
Published 1999Call Number: Loading…
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2
Unsteady ejector performance an experimental investigation using a pulsejet driver / by Paxson, Daniel E.
Published 2002Call Number: Loading…Connect to online resource
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3
A simplified model for detonation based pressure-gain combustors by Paxson, Daniel E.
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4
Ejector enhanced pulsejet based pressure gain combustors an old idea with a new twist / by Paxson, Daniel E.
Published 2005Call Number: Loading…Online Access
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5
A sectored-one-dimensional model for simulating combustion instabilities in premix combustors / by Paxson, Daniel E.
Published 1999Call Number: Loading…Online Access
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6
Performance impact of deflagration to detonation transition enhancing obstacles by Paxson, Daniel E.
Published 2012Call Number: Loading…Online Access
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7
Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines by Paxson, Daniel E.
Published 2012Call Number: Loading…Online Access
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8
An incidence loss model for wave rotors with axially aligned passages / by Paxson, Daniel E.
Published 1998Call Number: Loading…Online Access
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9
A comparison between numerically modelled and experimentally measured loss mechanisms in wave rotors by Paxson, Daniel E.
Published 1993Call Number: Loading…
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10
Examination of wave speed in rotating detonation engines using simplified computational fluid dynamics : prepared for 2018 SciTech Forum spnsored by the American Institute of Aeron... by Paxson, Daniel E.
Published 2018Call Number: Loading…Online Access
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11
An incidence loss model for wave rotors with axially aligned passages / by Paxson, Daniel E.
Published 1998Call Number: Loading…
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12
A general numerical model for wave rotor analysis by Paxson, Daniel E.
Published 1992Call Number: Loading…
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13
An improved numerical model for wave rotor design and analysis by Paxson, Daniel E.
Published 1992Call Number: Loading…
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14
Numerical analysis of a rotating detonation engine in the relative reference frame / by Paxson, Daniel E.
Published 2014Call Number: Loading…Online Access
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15
A model for the space shuttle main engine high pressure oxidizer turbopump shaft seal system by Paxson, Daniel E.
Published 1990Call Number: Loading…
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16
Recent improvements to and validation of the one dimensional NASA wave rotor model by Paxson, Daniel E.
Published 1995Call Number: Loading…
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17
Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / by Paxson, Daniel E.
Published 2015Call Number: Loading…Online Access
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18
Wave augmented diffusers for centrifugal compressors by Paxson, Daniel E.
Published 1998Call Number: Loading…
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19
Numerical assessment of four-part through-flow wave rotor cycles with passage height variation by Paxson, Daniel E.
Published 1997Call Number: Loading…
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20
A modified through-flow ware rotor cycle with combustor bypass ducts by Paxson, Daniel E.
Published 1998Call Number: Loading…
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Related Subjects
Computational fluid dynamics
Combustion chambers
Combustion
Flow distribution
Rotors
Gas turbine engines
Unsteady flow
Combustion stability
Detonation
Fuel flow
Heat transfer
Pulse detonation engines
Turboshafts
Wave rotors
Acoustic instability
Aerodynamics
Centrifugal compressors
Centrifugal force
Compression waves
Computerized simulation
Dynamic characteristics
Ejectors
Elastic waves
Equations of motion
Flow velocity
Fuel consumption
Gas turbines
Gas-turbines
Inlet pressure
Mathematical models