Comprehensive Validation of Skeletal Mechanism for Turbulent Premixed Methane–Air Flame Simulations
Steady-State Analysis of Rotating Detonation Engine Flowfields with the Method of Characteristics
Steady-State Analysis of Rotating Detonation Engine Flowfields with the Method of Characteristics
Microfabricated Electrospray Thruster Array with High Hydraulic Resistance Channels
Microfabricated Electrospray Thruster Array with High Hydraulic Resistance Channels
Experimental Study of Pressure Gain Combustion with Hypergolic Rocket Propellants
Measuring Propellant Stress Relaxation Modulus Using Dynamic Mechanical Analyzer
Flow Evolution Through a Turning Midturbine Frame with Embedded Design
Combustion Instability Suppression in Gaseous Oxygen/Hydrogen Combustors Using Methane Dilution
Combustion Instability Suppression in Gaseous Oxygen/Hydrogen Combustors Using Methane Dilution
Strut Injectors for Scramjets: Total Pressure Losses in Two Streamwise Vortex Interactions
Strut Injectors for Scramjets: Total Pressure Losses in Two Streamwise Vortex Interactions
Thermodynamic Modeling of a Rotating Detonation Engine Through a Reduced-Order Approach
Thermodynamic Modeling of a Rotating Detonation Engine Through a Reduced-Order Approach
Simulations of Ion Thruster Plumes in Ground Facilities Using Adaptive Mesh Refinement
Simulations of Ion Thruster Plumes in Ground Facilities Using Adaptive Mesh Refinement
Investigation of Channel Interactions in Nested Hall Thruster
Investigation of Channel Interactions in Nested Hall Thruster
Influence of the Tip Clearance on a Compressor Blade Aerodynamic Damping
Influence of the Tip Clearance on a Compressor Blade Aerodynamic Damping
Microcooling Channel Effect on a Monopropellant Microelectromechanical System Thruster Performance
Effects of Water-Vapor Propellant on Electrodeless Thruster Performance
Robustness of a Turbine Endwall Film Cooling Design to Swirling Combustor Inflow
Robustness of a Turbine Endwall Film Cooling Design to Swirling Combustor Inflow
Development of High-Frequency Pulse Detonation Combustor Without Purging Material
Development of High-Frequency Pulse Detonation Combustor Without Purging Material
Measurement of Impulsive Thrust from a Closed Radio-Frequency Cavity in Vacuum
Measurement of Impulsive Thrust from a Closed Radio-Frequency Cavity in Vacuum