| Considerations for Reducing Aviation's CO2 with Aircraft Electric Propulsion |
9 |
| Additive Manufacturing of Solid Rocket Propellant Grains |
7 |
| Hollow Cathode Simulations with a First-Principles Model of Ion-Acoustic Anomalous Resistivity |
7 |
| Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Nozzles |
7 |
| Large-Eddy Simulation of Reacting Flows in Industrial Gas Turbine Combustor |
6 |
| Electric Solid Propellant Ablation in an Arc Discharge |
6 |
| Optimization and Knowledge Discovery of a Three-Dimensional Parameterized Vane with Nonaxisymmetric Endwall |
6 |
| Performance Enhancement of a Small Two-Stroke Engine Using Nitromethane Blends |
5 |
| Inlet Distortion Effects on Fuel Distribution and Ignition in Scramjet Cavity Flameholder |
5 |
| Longitudinal Combustion Instability in a Rocket Engine with a Single Coaxial Injector |
5 |
| Mathematical Model of Dual-Pulse Laser Ignition |
5 |
| Role of Ignition Delay in Rotating Detonation Engine Performance and Operability |
5 |
| Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization |
5 |
| Improving Scramjet Performance Through Flow Field Manipulation |
5 |
| Fundamental Scramjet Combustion Experiments Using Hydrocarbon Fuel |
5 |
| Stabilization of Premixed Swirl Flames Under Flow Pulsations Using Microsecond Pulsed Plasmas |
4 |
| Simple Physics-Based Model for the Prediction of Shock-Train Location |
4 |
| Effect of Vibrational Nonequilibrium on Isolator Shock Structure |
4 |
| Direct Thrust Measurement of an Electron Cyclotron Resonance Plasma Thruster |
4 |
| Forced Response Analysis of a Mistuned Blisk Using Noncyclic Reduced-Order Models |
4 |
| Heat Transfer and Combustion Simulation of Seven-Element O-2/CH4 Rocket Combustor |
4 |
| Ignition of Hydrogen Peroxide with Gel Hydrocarbon Fuels |
4 |
| Fuel Regression Characteristics of a Novel Axial-Injection End-Burning Hybrid Rocket |
4 |
| Background Pressure Effects on Ion Velocity Distributions in an SPT-100 Hall Thruster |
4 |
| Aluminum Oxide-Supported Manganese Oxide Catalyst for a 98% Hydrogen Peroxide Thruster |
4 |
| Development of a Skeletal Mechanism for Aviation Kerosene Surrogate Fuel |
4 |
| Effects of Tip Clearance on Stall Inception in a Multistage Compressor |
4 |
| Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights |
4 |
| Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios |
4 |
| Agglomerate Sizing in Aluminized Propellants Using Digital Inline Holography and Traditional Diagnostics |
4 |
| High-to-Low Initial Sample Ratio of Hierarchical Kriging for Film Hole Array Optimization |
3 |
| Performance Sensitivities of Rotating Detonation Engines Installed onto Waverider Forebodies |
3 |
| Aging Effects on the Burning Rates of Composite Solid Propellants with Nano-Additives |
3 |
| Ion Thruster Operation with Carbon Nanotube Field Emission Cathode |
3 |
| Large-Eddy Simulation of Supersonic Hydrogen/Oxygen Combustion: Application to a Rocketlike Igniter |
3 |
| Freejet Testing of the HIFiRE 7 Scramjet Flowpath at Mach 7.5 |
3 |
| Numerical Investigation of Reacting Flow in a Methane Rocket Combustor: Turbulence Modeling |
3 |
| Numerical Simulation of Chemical Erosion in Vega Solid-Rocket-Motor Nozzles |
3 |
| Development and Flight Operation of a Miniature Ion Propulsion System |
3 |
| Combustion Characteristics of a Hydroxylammonium-Nitrate-Based Monopropellant Thruster with Discharge Plasma System |
3 |
| Optical Diagnostics in a High-Pressure Combustor with Gaseous Oxygen and Kerosene |
3 |
| Scaling Approach for Sub-Kilowatt Hall-Effect Thrusters |
3 |
| Influence of Single-Component Fuels on Gas-Turbine Model Combustor Lean Blowout |
3 |
| Boron-Metal Fluoride Reactive Composites: Preparation and Reactions Leading to Their Ignition |
3 |
| Assessment of Presumed/Transported Probability Density Function Methods for Rocket Combustion Simulations |
3 |
| Advancing the Microcathode Arc Thruster: Effect of the Ablative Anode |
3 |
| Single-Phase Instability in Non-Premixed Flames Under Liquid Rocket Engine Relevant Conditions |
3 |
| Parallel Simulation of Aerodynamic Instabilities in Transonic Axial Compressor Rotor |
3 |
| Robust Turbine Blade Optimization in the Face of Real Geometric Variations |
3 |
| Aerodynamic Design of Nozzles with Uniform Outflow for Hypervelocity Ground-Test Facilities |
3 |
