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
Suppression of Hard Start for Nontoxic Hypergolic Thruster Using
Influences of Inlet Geometry Modification on Scramjet Flow and Combustion Dynamics
Influences of Inlet Geometry Modification on Scramjet Flow and Combustion Dynamics
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
A unified analytical approach for the acoustic conceptual design of fans of modern aero-engines
A unified analytical approach for the acoustic conceptual design of fans of modern aero-engines
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
Effects of Tabbed-Nozzle on Pumping Performance of Incompressible Short Mixer–Ejector
Effects of Tabbed-Nozzle on Pumping Performance of Incompressible Short Mixer–Ejector
Comparison Between Excited Hydroxyl Radical and Blue Radiation from Hydrogen Rocket Combustion
Comparison Between Excited Hydroxyl Radical and Blue Radiation from Hydrogen Rocket Combustion
Effects of Recess on the Self-Pulsation Characteristics of Liquid-Centered Swirl Coaxial Injectors
Lanthanum Hexaaluminate Catalyst Support in a Hydrogen Peroxide Thruster
Lanthanum Hexaaluminate Catalyst Support in a Hydrogen Peroxide Thruster
Numerical Simulations of Mixing Enhancement in Subsonic Jet Using High-Momentum Synthetic Jets
Stall-Warning Approach Based on Aeroacoustic Principle
Stall-Warning Approach Based on Aeroacoustic Principle
Numerical Investigation of Heat and Mass Transfer on an Anti-Icing Inlet Cone
Experimental Investigation of Flow Distortion in an Auxiliary-Power-Unit-Style Inlet System
Experimental Investigation of Flow Distortion in an Auxiliary-Power-Unit-Style Inlet System
Effect of Self-Recirculation-Casing Treatment on High Pressure Ratio Centrifugal Compressor
Flight Validation of a Rotary-Valved Four-Cylinder Pulse Detonation Rocket
Predicting Lean Blowout Limit of Combustors Based on Semi-Empirical Correlation and Simulation
Effect of Self-Recirculation-Casing Treatment on High Pressure Ratio Centrifugal Compressor
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
Design Optimization of a Novel Boundary Layer Diverter for Semi-Submerged Inlets