| Nome |
# |
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Numerical analysis of paraffin-wax/oxygen hybrid rocket engines, file e3835328-a547-15e8-e053-a505fe0a3de9
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600
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Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers, file e3835313-0256-15e8-e053-a505fe0a3de9
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274
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Dual-bell nozzle with fluidic control of transition for space launchers, file 9e1537f7-d892-4bd5-8d28-86e2d23e2132
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185
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Numerical issues in modeling combustion instability by quasi-1D Euler equations, file e383531b-67ab-15e8-e053-a505fe0a3de9
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153
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Evolution of cooling-channel properties for varying aspect ratio, file e3835318-5c5a-15e8-e053-a505fe0a3de9
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111
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A design strategy for water-based noise suppression systems in liquid rocket engines firing tests, file eca636c7-ec9b-448e-b7ef-231812354294
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96
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Modeling of high density polyethylene regression rate in the simulation of hybrid rocket flowfields, file e3835323-4c06-15e8-e053-a505fe0a3de9
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88
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Numerical simulations of the internal ballistics of paraffin–oxygen hybrid rockets at different scales, file e383532e-e795-15e8-e053-a505fe0a3de9
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73
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Numerical Analysis of Nozzle Material Thermochemical Erosion in Hybrid Rocket Engines, file e3835311-e78c-15e8-e053-a505fe0a3de9
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46
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Trade-off analysis of high-aspect-ratio-cooling-channels for rocket engines, file e3835312-34c8-15e8-e053-a505fe0a3de9
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31
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Analysis of In-Flight Behavior of Truncated Plug Nozzles, file e3835311-b216-15e8-e053-a505fe0a3de9
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27
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Characterization of unsteadiness in an overexpanded planar nozzle, file e383532b-6ba2-15e8-e053-a505fe0a3de9
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27
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A computational tool for the design of hybrid rockets, file e383532e-e7b8-15e8-e053-a505fe0a3de9
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24
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Onset of Heat Transfer Deterioration in Supercritical Methane Flow Channels, file e3835311-f80f-15e8-e053-a505fe0a3de9
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23
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Numerical study of liquefied natural gas as a coolant in liquid rocket engines, file e3835312-0e0a-15e8-e053-a505fe0a3de9
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23
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Numerical approach for the estimation of throat heat flux in liquid rocket engines, file e3835329-956b-15e8-e053-a505fe0a3de9
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20
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A hybrid real/ideal gas mixture computational framework to capture wave propagation in liquid rocket combustion chamber conditions, file e383532c-ac86-15e8-e053-a505fe0a3de9
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20
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Chemical Erosion of Carbon-Phenolic Rocket Nozzles with Finite-Rate Surface Chemistry, file e3835312-2dd1-15e8-e053-a505fe0a3de9
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18
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Radius of curvature effects on throat thermochemical erosion in solid rocket motors, file e3835313-504c-15e8-e053-a505fe0a3de9
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17
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Coupled wall heat conduction and coolant flow analysis for liquid rocket engines, file e3835312-3086-15e8-e053-a505fe0a3de9
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16
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Coupled numerical simulation of wall heat conduction and coolant flow in liquid rocket engines, file e3835313-002e-15e8-e053-a505fe0a3de9
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16
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Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers, file e3835312-34ca-15e8-e053-a505fe0a3de9
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15
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Numerical simulations of fuel shape change and swirling flows in paraffin/oxygen hybrid rocket engines, file 669997f7-af0d-4fc0-932e-fd2aa5fa4a65
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13
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Cooling Channel Analysis of a LOX/LCH4 Rocket Engine Demonstrator, file e3835311-d176-15e8-e053-a505fe0a3de9
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13
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Effect of Cooling Channel Aspect Ratio on Rocket Thermal Behavior, file e3835311-d16d-15e8-e053-a505fe0a3de9
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12
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Supercritical methane heat transfer modeling in rocket engine cooling channels, file e3835313-0214-15e8-e053-a505fe0a3de9
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12
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A Numerical Model for Supercritical Flow in Rocket Engine Applications, file e3835313-0257-15e8-e053-a505fe0a3de9
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12
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NUMERICAL EVALUATION OF HEAT TRANSFER ENHANCEMENT IN ROCKET THRUST CHAMBERS BY WALL RIBS, file e3835311-d16b-15e8-e053-a505fe0a3de9
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11
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A numerical approach for the study of the gas-surface interaction in carbon-phenolic solid rocket nozzles, file e3835311-a862-15e8-e053-a505fe0a3de9
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10
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Parametric Analysis of Cooling Properties of Candidate Expander-Cycle Fuels, file e3835312-29ba-15e8-e053-a505fe0a3de9
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10
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Analysis on the effect of channel aspect ratio on rocket thermal behavior, file e3835313-0212-15e8-e053-a505fe0a3de9
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10
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Investigation of transcritical methane flow and heat transfer in curved cooling channels, file e3835313-0640-15e8-e053-a505fe0a3de9
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9
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Numerical analysis of paraffin-wax/oxygen hybrid rocket engines, file e383532b-daf1-15e8-e053-a505fe0a3de9
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9
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null, file e383532c-04dc-15e8-e053-a505fe0a3de9
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9
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Quasi-2D modeling of high-aspect-ratio-cooling-channel flows, file e3835313-068c-15e8-e053-a505fe0a3de9
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8
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Flow analysis of transcritical methane in rectangular cooling channels, file e3835313-0a31-15e8-e053-a505fe0a3de9
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8
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null, file e383531b-01da-15e8-e053-a505fe0a3de9
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8
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null, file e383531d-33d8-15e8-e053-a505fe0a3de9
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8
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Analysis of Curved-Cooling-Channel Flow and Heat Transfer in Rocket Engines, file e3835311-c513-15e8-e053-a505fe0a3de9
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7
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Numerical Modeling of GOX/HTPB Hybrid Rocket Flowfields and Comparison with Experiments, file e3835311-d171-15e8-e053-a505fe0a3de9
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7
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Experimental Investigation on Methane in Transcritical Conditions, file e3835311-d175-15e8-e053-a505fe0a3de9
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7
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Radiation and Roughness Effects on the Thermochemical Erosion of Ablative Materials in Rocket Nozzles, file e3835311-e723-15e8-e053-a505fe0a3de9
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7
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An Italian network to improve hybrid rocket performance: Strategy and results, file e3835312-29b9-15e8-e053-a505fe0a3de9
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7
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Development of Thrust Chamber Components for a System Analysis Tool, file e3835311-d173-15e8-e053-a505fe0a3de9
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6
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Plastic cubf.sat for micropropulsion and active debris removal test, file e3835312-26f3-15e8-e053-a505fe0a3de9
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6
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Numerical simulation of hybrid rocket engine flowfields, file e3835312-2ebf-15e8-e053-a505fe0a3de9
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6
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Coupled analysis of hot-gas and coolant flows in LOX/methane thrust chambers, file e3835313-0178-15e8-e053-a505fe0a3de9
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6
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CFD Analysis of Curved Cooling Channel Flow and Heat Transfer in Rocket Engines, file e3835313-0a0a-15e8-e053-a505fe0a3de9
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6
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Chemical reaction effects on heat loads of CH4/O2 and H2/O2 rockets, file e383531b-9f62-15e8-e053-a505fe0a3de9
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6
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Chemical Reaction Effects on Wall Heat Flux in Liquid Rocket Thrust Chambers, file e3835311-d172-15e8-e053-a505fe0a3de9
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5
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Ablative material behavior in oxygen/methane thruster environment, file e3835311-e72b-15e8-e053-a505fe0a3de9
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5
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CFD analysis of transcritical methane in rocket engine cooling channels, file e3835312-0273-15e8-e053-a505fe0a3de9
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5
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Near wall recombination eects on the prediction of heat flux in O2/CH4 combustion chambers, file e3835312-2ec0-15e8-e053-a505fe0a3de9
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5
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Parametric analysis of heat transfer to supercritical-pressure methane, file e3835312-3083-15e8-e053-a505fe0a3de9
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5
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Conditions for the occurrence of heat transfer deterioration in light hydrocarbons flows, file e3835312-34c7-15e8-e053-a505fe0a3de9
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5
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Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors, file e3835312-34c9-15e8-e053-a505fe0a3de9
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5
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CFD analysis of hybrid rocket Flowfields including fuel pyrolysis and nozzle erosion, file e3835313-4d72-15e8-e053-a505fe0a3de9
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5
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null, file e3835314-2e2c-15e8-e053-a505fe0a3de9
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5
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null, file e383532c-05c8-15e8-e053-a505fe0a3de9
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5
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Film cooling modeling in liquid rocket thrust chambers, file e383532c-bb08-15e8-e053-a505fe0a3de9
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5
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Design and evaluation of aerospike nozzles for an upper stage application., file e383532e-d1da-15e8-e053-a505fe0a3de9
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5
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Numerical analysis of film cooling in advanced rocket nozzles, file e3835311-c839-15e8-e053-a505fe0a3de9
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4
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Flow Separation Response to Unsteady External Disturbances in Dual Bell Nozzles, file e3835311-d174-15e8-e053-a505fe0a3de9
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4
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Numerical parametric analysis of dual-bell nozzle flows, file e3835311-d9d1-15e8-e053-a505fe0a3de9
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4
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Convective and radiative wall heat transfer in liquid rocket thrust chambers, file e383531a-e3e7-15e8-e053-a505fe0a3de9
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4
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Hybrid rockets with axial injector: port diameter effect on fuel regression rate, file e383531b-7a62-15e8-e053-a505fe0a3de9
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4
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Validation of conjugate heat transfer model for rocket cooling with supercritical methane, file e383531b-9f5f-15e8-e053-a505fe0a3de9
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4
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Driving mechanisms in low order modeling of longitudinal combustion instability, file e383531b-f8d0-15e8-e053-a505fe0a3de9
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4
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Characterization of unsteadiness in an overexpanded planar nozzle, file e3835320-f81c-15e8-e053-a505fe0a3de9
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4
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Experimental and numerical methods for radiative wall heat flux predictions in paraffin–based hybrid rocket engines, file e3835323-28ab-15e8-e053-a505fe0a3de9
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4
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Numerical investigation on radiative heat loads in liquid rocket thrust chambers, file e3835324-4e33-15e8-e053-a505fe0a3de9
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4
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Estimation of Throat Heat Flux in Liquid Rocket Engines, file e383532c-159f-15e8-e053-a505fe0a3de9
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4
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Modeling liquid rocket engine coolant flow and heat transfer in high roughness channels, file e383532f-351f-15e8-e053-a505fe0a3de9
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4
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Direct numerical simulation of turbulent flow in pipes with realistic large roughness at the wall, file dee78ece-f6a0-4b3e-b06b-e2bfe2ca4cdf
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3
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Low-order model studies of combustion instabilities in a DVRC combustor, file e3835311-d170-15e8-e053-a505fe0a3de9
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3
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Role of wall shape on the transition in axisymmetric dual-bell nozzles, file e3835311-d5ea-15e8-e053-a505fe0a3de9
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3
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Thermochemical erosion analysis for graphite/carbon-carbon rocket nozzles, file e3835311-d5f8-15e8-e053-a505fe0a3de9
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3
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A QUASI-2-D MODEL FOR THE PREDICTION OF THE WALL TEMPERATURE OF ROCKET ENGINE COOLING CHANNELS, file e3835312-0645-15e8-e053-a505fe0a3de9
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3
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An approximate Riemann solver for real gas parabolized Navier-Stokes equations, file e3835312-2697-15e8-e053-a505fe0a3de9
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3
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Carbon-carbon nozzle erosion and shape change in full-scale solid-rocket motors, file e3835312-3081-15e8-e053-a505fe0a3de9
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3
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Navier-Stokes Analysis of Scale Effects on Ablation in Carbon-Carbon Rocket Nozzles, file e3835312-5271-15e8-e053-a505fe0a3de9
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3
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Convective and radiative contributions to wall heat transfer in liquid rocket Engine thrust chambers, file e3835312-ad7a-15e8-e053-a505fe0a3de9
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3
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Transcritical Methane Flows in LRE Cooling Channels, file e3835313-017c-15e8-e053-a505fe0a3de9
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3
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Separation shock cutoff frequency in dual bell nozzles, file e3835317-890e-15e8-e053-a505fe0a3de9
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3
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System analysis of low frequency combustion instabilities in liquid rocket engines, file e3835317-8b65-15e8-e053-a505fe0a3de9
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3
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Radius of curvature effects on throat thermochemical erosion in solid rocket motors, file e383531b-7a6b-15e8-e053-a505fe0a3de9
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3
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Simulation of gaseous oxygen/hydroxyl-terminated polybutadiene hybrid rocket flowfields and comparison with experiments, file e383531b-9f64-15e8-e053-a505fe0a3de9
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3
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A multi-dimensional approach for low order modeling of combustion instability in a rocket combustor, file e383531c-2e00-15e8-e053-a505fe0a3de9
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3
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Numerical and experimental investigation of nozzle thermochemical erosion in hybrid rockets, file e383531c-bab4-15e8-e053-a505fe0a3de9
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3
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null, file e383531c-f696-15e8-e053-a505fe0a3de9
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3
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Analysis of thermal stratification impact on the design of cooling channels for liquid rocket engines, file e3835321-262e-15e8-e053-a505fe0a3de9
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3
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Systematic strategies for thermochemical model reduction in rocket propulsion applications, file e3835323-09e8-15e8-e053-a505fe0a3de9
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3
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Fluidic control of transition in a dual-bell nozzle, file e383532b-eb6c-15e8-e053-a505fe0a3de9
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3
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A sensitivity study on a cfd model for paraffin-based hybrid rockets, file e383532b-f0fb-15e8-e053-a505fe0a3de9
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3
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null, file e383532c-13ef-15e8-e053-a505fe0a3de9
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3
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Conjugate heat transfer analysis of rectangular cooling channels using modeled and direct numerical simulation of turbulence, file e383532e-7cac-15e8-e053-a505fe0a3de9
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3
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HEM modeling for subcritical flows in liquid rocket engine cooling systems, file e383532f-3bc2-15e8-e053-a505fe0a3de9
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3
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Analysis of Unsteady Supersonic Viscous Flows by a Shock Fitting Technique, file e3835311-9d73-15e8-e053-a505fe0a3de9
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2
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Methodology to solve flowfields of plug nozzles for future launchers, file e3835311-a14d-15e8-e053-a505fe0a3de9
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2
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Numerical analysis of three-dimensional flow of supercritical fluid in asymmetrically heated channels, file e3835311-c90c-15e8-e053-a505fe0a3de9
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2
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| Totale |
2.322 |