Comprehensive Validation of Skeletal Mechanism for Turbulent Premixed Methane–Air Flame Simulations
Viscosity and Regression Rate of Liquefying Hybrid Rocket Fuels
Details on the Mechanism of High-Frequency Swirl Coaxial Self-Pulsation
Poststall Airfoil Performance and Vertical-Axis Wind Turbines
Large-Eddy Simulation of Supercritical Combustion: Model Validation Against Gaseous
Code-Validation Scalar Measurements in High-Pressure Hydrogen-Added Methane Combustion
Code-Validation Scalar Measurements in High-Pressure Hydrogen-Added Methane Combustion
Unsteady Performance of Rotating Detonation Engines with Different Exhaust Nozzles
Unsteady Performance of Rotating Detonation Engines with Different Exhaust Nozzles
Hybrid Gas Generator for a Staged Hybrid Rocket Engine
Hybrid Gas Generator for a Staged Hybrid Rocket Engine
Suppression of Hard Start for Nontoxic Hypergolic Thruster Using H2O2 Oxidizer
Three-Dimensional Boundary Layer in a Turbine Blade Passage
Three-Dimensional Boundary Layer in a Turbine Blade Passage
Acoustic Analysis of Valveless Pulsejet Engines
Acoustic Analysis of Valveless Pulsejet Engines
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
Experimental and Numerical Performance Analysis of a Self-Starting Three-Dimensional Scramjet Intake
Boundary Layer Ingestion Propulsion Benefit for Transport Aircraft
Characterizing Propellants for Variable-Thrust/Specific Impulse Colloid Thrusters
Uncertainty Quantification for Fat-Tailed Probability Distributions in Aircraft Engine Simulations
Uncertainty Quantification for Fat-Tailed Probability Distributions in Aircraft Engine Simulations
Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Design of a Premixed Fuel–Oxidizer System to Arrest Flashback in a Rotating Detonation Engine
Design of a Premixed Fuel–Oxidizer System to Arrest Flashback in a Rotating Detonation Engine
Flow Rate Measurement Method for Gaseous Fuel Injection for Pulse Detonation Engines
Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure
Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure
Effect of Azimuthally Nonuniform Heat Release on Longitudinal Combustion Instabilities
Effect of Azimuthally Nonuniform Heat Release on Longitudinal Combustion Instabilities
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
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
Suppression of Hard Start for Nontoxic Hypergolic Thruster Using