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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Propulsion and Power US/2008/4/

Folder.. - Mar 06 2025 12:36:30 AM
Ablative Impulse Characteristics of Polyacetal with Repetitive CO2 Laser Pulses.pdfAblative Impulse Characteristics of Polyacetal with Repetitive CO2 Laser Pulses.pdf 9298KB Mar 21 2010 12:53:36 PM
Adaptive Estimation Algorithm for Aircraft Engine Performance Monitoring.pdfAdaptive Estimation Algorithm for Aircraft Engine Performance Monitoring.pdf 2272KB Mar 21 2010 12:53:36 PM
Analytical Computation of Leading-Edge Truncation Effects on Inviscid Busemann-Inlet Performance.pdfAnalytical Computation of Leading-Edge Truncation Effects on Inviscid Busemann-Inlet Performance.pdf 1933KB Mar 21 2010 12:53:36 PM
Chemical Erosion of Carbon-Carbon Graphite Nozzles in Solid-Propellant Rocket Motors.pdfChemical Erosion of Carbon-Carbon Graphite Nozzles in Solid-Propellant Rocket Motors.pdf 4265KB Mar 21 2010 12:53:36 PM
Combustion Instability Problems Analysis for High-Pressure Jet Engine Cores.pdfCombustion Instability Problems Analysis for High-Pressure Jet Engine Cores.pdf 2797KB Mar 21 2010 12:53:36 PM
Complex Wall Injector Array for High-Speed Combustors.pdfComplex Wall Injector Array for High-Speed Combustors.pdf 8784KB Mar 21 2010 12:53:36 PM
Computational Methodology for Carbon Monoxide Emission for Aeroengine Combustor Design.pdfComputational Methodology for Carbon Monoxide Emission for Aeroengine Combustor Design.pdf 1722KB Mar 21 2010 12:53:36 PM
Computational Study on the Critical Nozzle Flow of High-Pressure Hydrogen Gas.pdfComputational Study on the Critical Nozzle Flow of High-Pressure Hydrogen Gas.pdf 996KB Mar 21 2010 12:53:36 PM
Effect of Liquid Injection on Acoustic Field Induced from Supersonic Flow Past Cavities.pdfEffect of Liquid Injection on Acoustic Field Induced from Supersonic Flow Past Cavities.pdf 9289KB Mar 21 2010 12:53:36 PM
Effects of Propellant Gases on Thermal Response of Solid Rocket Nozzle Liners.pdfEffects of Propellant Gases on Thermal Response of Solid Rocket Nozzle Liners.pdf 11916KB Mar 21 2010 12:53:36 PM
Electron Dynamics After Exit Plane of Stationary Plasma Thruster Discharge Chamber.pdfElectron Dynamics After Exit Plane of Stationary Plasma Thruster Discharge Chamber.pdf 541KB Mar 21 2010 12:53:36 PM
Erratum for Expectations of Closed-Brayton-Cycle Heat Exchangers in Space Power Systems.pdfErratum for Expectations of Closed-Brayton-Cycle Heat Exchangers in Space Power Systems.pdf 24KB Mar 21 2010 12:53:36 PM
Experimental and Numerical Investigation of n-Heptane Air Counterflow Nonpremixed Flame Structure.pdfExperimental and Numerical Investigation of n-Heptane Air Counterflow Nonpremixed Flame Structure.pdf 1194KB Mar 21 2010 12:53:36 PM
Experimental Study of a Scramjet Nozzle Flow Using the Pressure-Sensitive-Paint Method.pdfExperimental Study of a Scramjet Nozzle Flow Using the Pressure-Sensitive-Paint Method.pdf 14443KB Mar 21 2010 12:53:36 PM
Exploring the Effects of Removing Process-Intrinsic Constraints on Gas Turbine Design.pdfExploring the Effects of Removing Process-Intrinsic Constraints on Gas Turbine Design.pdf 3446KB Mar 21 2010 12:53:36 PM
Extraction of One-Dimensional Flow Properties from Multidimensional Data Sets.pdfExtraction of One-Dimensional Flow Properties from Multidimensional Data Sets.pdf 5598KB Mar 21 2010 12:53:36 PM
Flame Characteristics in Supersonic Combustor with Hydrogen Injection Upstream of Cavity Flameholder.pdfFlame Characteristics in Supersonic Combustor with Hydrogen Injection Upstream of Cavity Flameholder.pdf 10514KB Mar 21 2010 12:53:36 PM
Hydrocarbon Fuel Flash Vaporization for Pulsed Detonation Combustion.pdfHydrocarbon Fuel Flash Vaporization for Pulsed Detonation Combustion.pdf 897KB Mar 21 2010 12:53:36 PM
Ignition of Iron-Coated and Nickel-Coated Aluminum Particles Under Normal- and Reduced-Gravity Conditions.pdfIgnition of Iron-Coated and Nickel-Coated Aluminum Particles Under Normal- and Reduced-Gravity Conditions.pdf 15602KB Mar 21 2010 12:53:36 PM
Increasing Gas Turbine Blade Damping Through Cavities Filled with Viscoelastic Materials.pdfIncreasing Gas Turbine Blade Damping Through Cavities Filled with Viscoelastic Materials.pdf 5225KB Mar 21 2010 12:53:36 PM
Inexpensive Optically Isolated Nanoammeter for Use with Micro-Newton Electric Propulsion Technology.pdfInexpensive Optically Isolated Nanoammeter for Use with Micro-Newton Electric Propulsion Technology.pdf 680KB Mar 21 2010 12:53:36 PM
Ion-Collision Emission Excitation Cross Sections for Xenon Electric Thruster Plasmas.pdfIon-Collision Emission Excitation Cross Sections for Xenon Electric Thruster Plasmas.pdf 658KB Mar 21 2010 12:53:36 PM
Leakage Assessment of Pressure-Exchange Wave Rotors.pdfLeakage Assessment of Pressure-Exchange Wave Rotors.pdf 6778KB Mar 21 2010 12:53:36 PM
Observation of Unsteady Cryogenic Flows from a Characteristic Coaxial Rocket Injector.pdfObservation of Unsteady Cryogenic Flows from a Characteristic Coaxial Rocket Injector.pdf 564KB Mar 21 2010 12:53:36 PM
Passive Control Techniques to Alleviate Supersonic Cavity Flow Oscillation.pdfPassive Control Techniques to Alleviate Supersonic Cavity Flow Oscillation.pdf 6454KB Mar 21 2010 12:53:36 PM
Plasma-Assisted Ignition in Scramjets.pdfPlasma-Assisted Ignition in Scramjets.pdf 9881KB Mar 21 2010 12:53:36 PM
Role of Superconducting Shields in Electrodynamic Propulsion.pdfRole of Superconducting Shields in Electrodynamic Propulsion.pdf 609KB Mar 21 2010 12:53:36 PM
Unsteady Strong Shock Interactions in a Transonic Turbine_ Experimental and Numerical Analysis.pdfUnsteady Strong Shock Interactions in a Transonic Turbine_ Experimental and Numerical Analysis.pdf 9310KB Mar 21 2010 12:53:36 PM
Wear Mechanisms in Electron Sources for Ion Propulsion, II_ Discharge Hollow Cathode.pdfWear Mechanisms in Electron Sources for Ion Propulsion, II_ Discharge Hollow Cathode.pdf 1526KB Mar 21 2010 12:53:36 PM
Wear Mechanisms in Electron Sources for Ion Propulsion, I_ Neutralizer Hollow Cathode.pdfWear Mechanisms in Electron Sources for Ion Propulsion, I_ Neutralizer Hollow Cathode.pdf 3944KB Mar 21 2010 12:53:36 PM