Journal of Propulsion and Power

Article	Citations
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy	32
Announcements and Acknowledgements	29
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant	28
Expandable Graphite, a Novel Regression Rate Enhancer in the Solid Fuel Ramjet	26
Experimental Comparison of Jet Modes Using Self-Excited Sweeping Jet Actuator in Compressor Cascades	25
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver	23
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization	23
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine	19
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	18
Correlation for Restart Boundaries of Simplified Two-Dimensional Hypersonic Inlets	18
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics	17
Preparation, Ignition, and Combustion of Boron Fuels with CuO as an Additive	17
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels	17
Characterizing Hypergolic Propellants Using Impinging Jets and Droplets in Acoustic Levitation	16
Simulation of Vacuum Chamber Pressure Distributions with Uncertainty Quantification	15
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers	15
Dynamic Regulation Process of the Variable-Geometry Power Turbine	15
Structure and Stabilization Mechanisms of an Ethylene Flame in Supersonic Coflow	14
Firing Tests and Simulations of a CubeSat-Scale H2O2-Based Hybrid Rocket	14
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion	13
Data-Driven Wall Pressure Reconstruction and Sparse Sensor Optimization for Supersonic Nozzles	13
Combustion of 3D Printable Hybrid Rocket Fuels	13
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability	13
Stochastic Emission in Passively Fed Single-Emitter Porous-Media Ionic Liquid Ion Sources	13
Improved Response Function for Low-Order Modeling of Longitudinal Combustion Instabilities	12

General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants	11
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities	11
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor	11
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge	11
Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology	11
Loss Mechanisms of Shrouded Stator Cavity Flow in an Axial Compressor	11
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets	11
Effect of Varying Secondary Swirl Injector Location on Performance of Hybrid Rocket	11
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet	10
Surface Structure of Reacting Solid Ramjet Fuels	10
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests	10
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor	9
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet	9
Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles	9
Effect of Fuel Injection Strategy on Generic Scramjet Combustor Operation	9
Pilot Injection Impact on Ignition of F-24/ATJ Blends Under Various Conditions	9
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor	9
Thermal and Resonance Characteristics of Tapered Cavities of Various Lengths	9
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels	8
Multipoint Aerodynamic Optimization of Three-Dimensional Ultra-High-Bypass-Ratio Engine Intakes	8
Uncertainty Quantification of Slab Burner Simulation: Surrogates, Forward Propagation, and Parameter Calibration	8
Performance of Novel Electrode Structures for Electrically Controlled Solid Propellant	8
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide	8
Combustion of Preheated Hydrocarbon Fuel in a Scramjet Model Combustor	8
Effects of Evaporation Modeling on Kerosene–Air Oblique Detonation	8
Characterization of a Nanonewton-Sensitivity Counterbalanced Pendulum Thrust Stand for Pulsed Propulsion Systems	7
Reducing Aluminum Agglomeration in Composite Propellants with Gallium and Indium Additives	7
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan	7
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection	7
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants	7
Injection Temperature and Scheme Effects on Neutral Flow Dynamics in Hall Thrusters	7
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles	7
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation	7
Evaluation of Radiative Heat-Transfer Effect on Paraffin-Wax Regression Rate in Hybrid Rocket	7
Erosion Mechanisms of Baffle Plates at Stagnation Point in Hybrid Rockets	7
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing	7
Unraveling the Transition from Standard to Reactive Atomization of Hypergolic Propellants	6
Supersonic Combustion and Flow Evolution in Dual-Combustion Ramjet Engine	6
Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets Using LOX	6
Interaction Behavior of Pulsejet Engines	6
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets	6
Delayed Detached-Eddy Simulations of Rough-Wall Turbulent Reactive Flows in a Supersonic Combustor	6
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake	6
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws	6
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations	5
Beam Misalignment Effects on Microwave Rocket Propulsion Performance	5
Performance Test of a Diode Laser-Sustained Plasma Thruster Using Argon	5
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power	5
Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking	5
Characterizing the Oscillatory Unstart/Restart of a Supersonic Stator in Unsteady Conditions	5

Low-Order Autoignition Modeling for Hydrogen Transverse Jets	5
Flame Structures in a Model Solid Fuel Ramjet with Increasing Reynolds Numbers	5
Data-Driven Analysis of Tortuous Gas Turbine Inlet Truncation to Reduce Computational Cost	5
Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine	5
Design of an Internal Osculating Waverider Intake	5
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates	5
Control of Shock-Induced Flow Separation Using Rectangular Air-Jet Vortex Generators	5
High-Specific-Impulse Electrospray Propulsion with Small Capillary Emitters	5
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator	5
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype	5
Announcements and Acknowledgements	4
Combustion Instability Characteristics of a Methane–Oxygen Shear Tri-Coaxial Rocket Injector	4
Improving Detonability in a Small-Scale Rotating Detonation Engine Using Partial Premixing	4
Performance of Water-Augmented Metallized Hybrid Propellant Ram Rocket During Underwater Motion	4
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters	4
Parametric Analysis of Hydrogen Swirl Combustors with Incompletely Stirred Reactor Network Modeling	4
Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition	4
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine	4
Announcements and Acknowledgments	4
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine	4
Microthrusters’ Combustion Control Using Jellied Propellant Flowing Through an Orifice Plate	4
Correction: Comparison of Turbulence and Chemistry Closures in a Solid Fuel Ramjet Combustor	4
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications	4
Steady-State and Pulsed Performance Results of a Tripropellant Autophage Engine Architecture	4
Development and Evaluation of Reduced Kinetics Models for 1,3-Butadiene–Air Combustion	4
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics	4
Study of Boron Fuel in a Water-Breathing Ramjet	4
Parameter Influence on Porous Bleed Performance for Supersonic Turbulent Flows	4
Hall Thruster System Using Dry Ice Propellant at the Triple Point	4
Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment	4
Solid-Fuel Ramjet Regression Rate Measurements Using X-Ray Radiography and Ultrasonic Transducers	3
Stall Inception of Axial Fan with Foam Metal Casing Treatment	3
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor	3
Flame-Spreading Process in Solid Rocket Motor with Fin Slots	3
Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine	3
Lagrangian Simulation Methodology for Large-Eddy Simulations of Prefilming Air-Blast Injectors	3
Methodology for Assessing Retrofitted Hydrogen Combustion and Fuel Cell Aircraft Environmental Impacts	3
Deflagration to Detonation Transition in Heterogeneous Mixtures Containing Ethanol/Acetone and Oxygen	3
Simulated Scramjet Shock Train Control Using an All-Coefficient Adaptive Control Approach	3
Seven-Zone Parametric Optimization Method for Compressor Profile with Controllable Maximum Thickness	3
Processing and Testing Subscale Motors with Central Finocyl Grain Using Wax Mandrel	3
Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement	3
Ejector Recirculation and Entrainment	3
Statistical Characterization of Emitter Fabrication over Electrospray Array Thruster	3
Observation of Plasma Turbulence in a Hall Thruster Using Microwave Interferometry	3
Inlet Guide Vane Stagger Effects on Multistage Compressor Performance and Stall Inception	3
Reducing Preheating Requirements for 1-N-Scale Thruster with Ammonium Dinitramide-H2O2 Monopropellant	3
Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants	3
Study on the Design Methodology of Turbine Profiles Operating Within Wide-Inflow-Angle Ranges	3
Liquid Column Separation Due to Fluid Hammer Occurrence in Propellant Lines	3
Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant	3
Numerical Analysis of a Novel Casing Treatment in an Axial Flow Fan	3
Assessment of Pseudoshock Models Against Experiment in a Low-Aspect-Ratio Isolator	3
Extinguishing and Combustion Characteristics of Electrically Controllable Solid Propellants Under Elevated Pressures	3
Electrospray Characteristics of High-Energetic Ionic Liquids: Ammonium Dinitramide and Hydroxyethylhydrazinium Nitrate	3
Similarity and Scaling in a Liquid-Fuel Ramjet Combustor	3
Effects of Thermal Expansion and Pressure on Far-Field Fluctuations of Heterogeneous Propellants	3
Numerical Estimation of Nozzle Throat Heat Flux in Oxygen-Methane Rocket Engines	3
Electrically Controlled Ignition Performance of LiClO4/PVA/H2O Propellants	3
Computational Study on Fully Coupled Combustor–Turbine Interactions	3
Evaluating the Effects of Fill Height in a Narrow Detonation Channel	3
Performance Scaling of Modular Hybrid Propulsion System for Flight Vehicles	3
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions	3
Active Energy Management for Enhanced Engine Transient Operations	2
Multiple Diagnostics of Hybrid Rocket Ignition and Effect of Hypergolic Additive Granulometry	2
Propellant Surface Evolution of a Coaxial Pulsed Plasma Thruster	2
Computational Study of Propulsive Performance of Frozen Nano-Aluminum and Water (ALICE) Mixtures	2
Synchronized Initiation of Two Cylindrical Rotating Detonation Engines	2
Effect of Nonuniform Plasma on Grid Erosion of the Water Ion Thruster	2
Implicit Simulation of Turbomachinery Flows on Structured Meshes Using Graphics Processing Units	2
Study of Suborbital Rocket Plane Using Highly Pressurized Hydrogen/Nitrous Oxide	2
Fuel Injector Requirements to Achieve Supercritical Flow at the Exit	2
High-Pressure Combustion Characteristics of Hydroxyl-Terminated Polybutadiene Propellants	2
Optimized Postprocessing Method for Fatigue Life Evaluation of Reusable Rocket Combustion Chambers	2
Liquid Atomization in Rotary Slinger Injectors: Role of Liquid Delivery Manifold	2
Hypergolic Properties of Solvated Lithium, Sodium, and Calcium in Liquid Anhydrous Ammonia	2
Tandem Energy-Analyzer/Mass-Spectrometer Measurements of an Ionic Liquid Ion Source	2
Demonstration of One Hundred Kilogram Xenon Throughput by a Low-Power Hall Thruster	2
Announcements and Acknowledgements	2
Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes	2

Improving Base-Drag Corrections for Rotating Detonation Combustor Gross Thrust Measurements	2
Performance Impacts of Preheating the Primary Fuel Jet of an Ejector Ramjet	2
Novel Hypergolic Green Fuels with Hydrogen Peroxide for Propulsion Systems	2
Quantification of Heat Loads in Rotating Detonation Combustors for Gas Turbines	2
Effect of Boric Acid on Electronically Controlled Solid Propellants	2