Comprehensive Validation of Skeletal Mechanism for Turbulent Premixed Methane–Air Flame Simulations
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
Numerical Analysis of Curved Thrusters for Multichamber Aerospike Engines in Flight Conditions
Numerical Analysis of Curved Thrusters for Multichamber Aerospike Engines in Flight Conditions
Rate-Controlled Constrained Equilibrium for Nozzle and Shock Flows
Rate-Controlled Constrained Equilibrium for Nozzle and Shock Flows
Combustion Dynamics in Postchamber of Hybrid Rocket Using CH Radical Chemiluminescence Images
Chemical-Equilibrium Analysis with Adjoint Derivatives for Propulsion Cycle Analysis
Chemical-Equilibrium Analysis with Adjoint Derivatives for Propulsion Cycle Analysis
Background Flow Model of Hall Thruster Neutral Ingestion
Background Flow Model of Hall Thruster Neutral Ingestion
Influences of Inlet Geometry Modification on Scramjet Flow and Combustion Dynamics
Influences of Inlet Geometry Modification on Scramjet Flow and Combustion Dynamics
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
AIAA Policy Statements and Manuscript Review Process