Beam-Riding Flight of a Laser Propulsion Vehicle Using Actively Controlled Pulse
Beam-Riding Flight of a Laser Propulsion Vehicle Using Actively Controlled Pulse
Electrolytic Combustion in the Polyvinyl Alcohol Plus Hydroxylammonium Nitrate Solid Propellant
Creep-Life Usage Analysis and Tracking for Industrial Gas Turbines
Journal of Propulsion and Power 2017 Chronological Index
Large-Eddy Simulation of Supercritical Combustion: Model Validation Against Gaseous H2–O2 Injector
Excessively Fuel-Rich Conditions for Cold Starting of Liquid-Fuel Pulse Detonation Engines
Excessively Fuel-Rich Conditions for Cold Starting of Liquid-Fuel Pulse Detonation Engines
Disturbance-Field Decomposition in a Transversely Forced Swirl Flow and Flame
Disturbance-Field Decomposition in a Transversely Forced Swirl Flow and Flame
The Rayleigh Efficiency of Pressure Gain Combustors
The Rayleigh Efficiency of Pressure Gain Combustors
Flow Characterization for a Shallow Single Serpentine Nozzle with Aft Deck
Flow Characterization for a Shallow Single Serpentine Nozzle with Aft Deck
Thrust Control by Fluidic Injection in Solid Rocket Motors
Thrust Control by Fluidic Injection in Solid Rocket Motors
High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations
High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations
Strut Injectors for Scramjets: Total Pressure Losses in Two Streamwise Vortex Interactions
Strut Injectors for Scramjets: Total Pressure Losses in Two Streamwise Vortex Interactions
Journal of Propulsion and Power 2017 Author Index
Investigation of Channel Interactions in Nested Hall Thruster
Investigation of Channel Interactions in Nested Hall Thruster
Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Introduction: Special Section on Pressure Gain Combustion
Impact of Weld Joint on Compressor Blade Performance
Impact of Weld Joint on Compressor Blade Performance
Experimental and Numerical Performance Analysis of a Self-Starting Three-Dimensional Scramjet Intake
Boundary Layer Ingestion Propulsion Benefit for Transport Aircraft