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
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
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
Measurement of Impulsive Thrust from a Closed Radio-Frequency Cavity in Vacuum
Measurement of Impulsive Thrust from a Closed Radio-Frequency Cavity in Vacuum
Simulations of Ion Thruster Plumes in Ground Facilities Using Adaptive Mesh Refinement
Simulations of Ion Thruster Plumes in Ground Facilities Using Adaptive Mesh Refinement
Diffusion-Flame Ignition by Shock-Wave Impingement on a Hydrogen–Air Supersonic Mixing Layer
Combustion Dynamics in Postchamber of Hybrid Rocket Using
Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor
Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor
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
Suppression of Hard Start for Nontoxic Hypergolic Thruster Using
Shock Tube Experimental Studies on CH/Visible Light/Pressure as Ignition Delay Criteria
Shock Tube Experimental Studies on CH/Visible Light/Pressure as Ignition Delay Criteria
Comparative Study of Mixing Characteristics of Particle-Laden Shear and Swirl Coaxial Jets
Comparative Study of Mixing Characteristics of Particle-Laden Shear and Swirl Coaxial Jets
Overview of Performance, Application, and Analysis of Rotating Detonation Engine Technologies
Flow Analysis of a Helicopter Engine Side Air Intake
Flow Analysis of a Helicopter Engine Side Air Intake
Blade-Row Interaction Effects on Unsteady Stator Loading in an Embedded Compressor Stage
Blade-Row Interaction Effects on Unsteady Stator Loading in an Embedded Compressor Stage
Effect of Azimuthally Nonuniform Heat Release on Longitudinal Combustion Instabilities
Effect of Azimuthally Nonuniform Heat Release on Longitudinal Combustion Instabilities
Effect of Preinducer in Reducing Net Positive Suction Head Requirement of a Pump
Effect of Preinducer in Reducing Net Positive Suction Head Requirement of a Pump
Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines
Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines