Fuel Temperature Effects on Combustion Stability of a High-Pressure Liquid-Fueled Swirl Flame

2024-9-12

Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles

2024-9-12

Enhancing Hybrid Rocket Engine Regression Rates: The Stepped Helix Design

2024-9-1

General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants

2024-9-1

Optimization of Thrust of a Generic X-51 Hypersonic Vehicle

2024-8-23

Application of Boundary Layer Combustion in High-Mach-Number Scramjets

2024-8-13

Active Energy Management for Enhanced Engine Transient Operations

2024-7-14

Monodisperse Porous Emitter Materials for Ion Electrospray Propulsion

2024-7-9

Numerical Analysis of a Novel Casing Treatment in an Axial Flow Fan

2024-7-1

Optimal Liquid Engine Architecture by Performance-Cooling Tradeoff Analysis

2024-7-1

Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants

2024-7-1

Multiple Diagnostics of Hybrid Rocket Ignition and Effect of Hypergolic Additive Granulometry

2024-6-25

Effect of Boric Acid on Electronically Controlled Solid Propellants

2024-6-20

Synchronized Initiation of Two Cylindrical Rotating Detonation Engines

2024-6-20

Tandem Energy-Analyzer/Mass-Spectrometer Measurements of an Ionic Liquid Ion Source

2024-5-28

Propagating an Electrospray Emission Model to Array Scales Using Particle-in-Cell

2024-5-21

Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine

2024-5-21

Shear Coaxial Methane–Oxygen Injector Mixing and Combustion Examined by Laser Absorption Tomography

2024-5-12

Optimization and Testing of DC Electromagnetic Pump for Liquid Metal Space Use

2024-5-8

High-Current Density Performance of a Magnetically Shielded Hall Thruster

2024-5-2

Delayed Detached-Eddy Simulations of Rough-Wall Turbulent Reactive Flows in a Supersonic Combustor

2024-5-1

Current Status of Liquid-Bipropellant Detonation-Based Propulsion Devices

2024-5-1

Continuous Injector Geometry Variation to Augment Rotating Detonation Combustor Operation and Performance

2024-5-1

Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype

2024-5-1

Experimental Study on Infrared Radiation Characteristics and Matching Performance of Low-Observable Nozzles

2024-5-1

Supersonic Combustion of Solid Fuels

2024-5-1

Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation

2024-5-1

Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology

2024-5-1

High-Voltage Discharge Optimization of a Hybrid-Wall Hall Thruster

2024-4-30

Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition

2024-4-25

Investigation of Unsteady Combustion Regimes in a Kerosene-Fueled Scramjet with Air Throttling

2024-4-10

Effects of Thermal Expansion and Pressure on Far-Field Fluctuations of Heterogeneous Propellants

2024-4-5

Methodology for Assessing Retrofitted Hydrogen Combustion and Fuel Cell Aircraft Environmental Impacts

2024-4-5

Inlet Guide Vane Stagger Effects on Multistage Compressor Performance and Stall Inception

2024-3-11

Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section

2024-3-1

Fuel Injector Requirements to Achieve Supercritical Flow at the Exit

2024-3-1

Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels

2024-3-1

Novel Hypergolic Green Fuels with Hydrogen Peroxide for Propulsion Systems

2024-3-1

Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion

2024-3-1

Hypersonic International Flight Research Experimentation Flight 2 Unstart Reliability Analysis

2024-3-1

Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities

2024-3-1

Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics

2024-3-1

Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet

2024-3-1

Optimization of Rotor Tip Cavity Shapes for Mitigating Aerodynamic Tip Leakage Losses

2024-3-1

Performance Evaluation of Damaged Blades Using Numerical Simulation and Machine Learning

2024-3-1

Liquid Atomization in Rotary Slinger Injectors: Role of Liquid Delivery Manifold

2024-2-29

Simplified Data-Reduction Method for Hybrid Propulsion

2024-2-29

Beam Misalignment Effects on Microwave Rocket Propulsion Performance

2024-2-13

Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets

2024-2-13

Novel Solid Propellants Enabled Through In Situ Martian Perchlorates

2024-2-13