Journal of Propulsion and Power

Article	Citations
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy	37
Announcements and Acknowledgements	32
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant	29
Correlation for Restart Boundaries of Simplified Two-Dimensional Hypersonic Inlets	28
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver	27
Expandable Graphite, a Novel Regression Rate Enhancer in the Solid Fuel Ramjet	27
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine	26
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	21
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization	20
Experimental Comparison of Jet Modes Using Self-Excited Sweeping Jet Actuator in Compressor Cascades	20
Combustion of 3D Printable Hybrid Rocket Fuels	19
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics	19
Preparation, Ignition, and Combustion of Boron Fuels with CuO as an Additive	19
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels	18
Characterizing Hypergolic Propellants Using Impinging Jets and Droplets in Acoustic Levitation	18
Simulation of Vacuum Chamber Pressure Distributions with Uncertainty Quantification	17
Structure and Stabilization Mechanisms of an Ethylene Flame in Supersonic Coflow	17
Firing Tests and Simulations of a CubeSat-Scale H2O2-Based Hybrid Rocket	17
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers	16
Improved Response Function for Low-Order Modeling of Longitudinal Combustion Instabilities	15
Dynamic Regulation Process of the Variable-Geometry Power Turbine	15
Stochastic Emission in Passively Fed Single-Emitter Porous-Media Ionic Liquid Ion Sources	14
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability	14
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion	14
Data-Driven Wall Pressure Reconstruction and Sparse Sensor Optimization for Supersonic Nozzles	14

Loss Mechanisms of Shrouded Stator Cavity Flow in an Axial Compressor	13
Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology	13
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities	13
Effect of Varying Secondary Swirl Injector Location on Performance of Hybrid Rocket	13
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge	13
General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants	12
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests	12
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor	12
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor	12
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet	12
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets	12
Surface Structure of Reacting Solid Ramjet Fuels	11
Pilot Injection Impact on Ignition of F-24/ATJ Blends Under Various Conditions	11
Uncertainty Quantification of Slab Burner Simulation: Surrogates, Forward Propagation, and Parameter Calibration	11
Multipoint Aerodynamic Optimization of Three-Dimensional Ultra-High-Bypass-Ratio Engine Intakes	11
Effects of Evaporation Modeling on Kerosene–Air Oblique Detonation	11
Effect of Fuel Injection Strategy on Generic Scramjet Combustor Operation	11
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet	11
Combustion of Preheated Hydrocarbon Fuel in a Scramjet Model Combustor	11
Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles	10
Thermal and Resonance Characteristics of Tapered Cavities of Various Lengths	10
Performance of Novel Electrode Structures for Electrically Controlled Solid Propellant	9
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide	9
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor	9
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels	9
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants	8
Reducing Aluminum Agglomeration in Composite Propellants with Gallium and Indium Additives	8
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation	8
Injection Temperature and Scheme Effects on Neutral Flow Dynamics in Hall Thrusters	8
Characterization of a Nanonewton-Sensitivity Counterbalanced Pendulum Thrust Stand for Pulsed Propulsion Systems	8
Evaluation of Radiative Heat-Transfer Effect on Paraffin-Wax Regression Rate in Hybrid Rocket	8
Erosion Mechanisms of Baffle Plates at Stagnation Point in Hybrid Rockets	8
Experimental Study of a Cylindrical Rotating Detonation Combustor for Scramjet Ignition	8
Supersonic Combustion and Flow Evolution in Dual-Combustion Ramjet Engine	7
Low-Order Autoignition Modeling for Hydrogen Transverse Jets	7
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing	7
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake	7
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan	7
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations	7
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection	7
Unraveling the Transition from Standard to Reactive Atomization of Hypergolic Propellants	7
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets	7
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles	7
Interaction Behavior of Pulsejet Engines	7
Flame Structures in a Model Solid Fuel Ramjet with Increasing Reynolds Numbers	6
Delayed Detached-Eddy Simulations of Rough-Wall Turbulent Reactive Flows in a Supersonic Combustor	6
Beam Misalignment Effects on Microwave Rocket Propulsion Performance	6
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates	6
Data-Driven Analysis of Tortuous Gas Turbine Inlet Truncation to Reduce Computational Cost	6
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws	6

Characterizing the Oscillatory Unstart/Restart of a Supersonic Stator in Unsteady Conditions	6
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power	6
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype	6
Control of Shock-Induced Flow Separation Using Rectangular Air-Jet Vortex Generators	6
Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets Using LOX	6
Performance Test of a Diode Laser-Sustained Plasma Thruster Using Argon	6
Design of an Internal Osculating Waverider Intake	6
High-Specific-Impulse Electrospray Propulsion with Small Capillary Emitters	6
Announcements and Acknowledgements	5
Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition	5
Hall Thruster System Using Dry Ice Propellant at the Triple Point	5
Announcements and Acknowledgments	5
Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine	5
Parametric Analysis of Hydrogen Swirl Combustors with Incompletely Stirred Reactor Network Modeling	5
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters	5
Steady-State and Pulsed Performance Results of a Tripropellant Autophage Engine Architecture	5
Combustion Instability Characteristics of a Methane–Oxygen Shear Tri-Coaxial Rocket Injector	5
Development and Evaluation of Reduced Kinetics Models for 1,3-Butadiene–Air Combustion	5
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications	5
Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment	5
Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking	5
Correction: Comparison of Turbulence and Chemistry Closures in a Solid Fuel Ramjet Combustor	5
Performance Characterization of Electrospray Thrusters with Energetic Ionic Liquid Monopropellant	5
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine	5
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine	5
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator	5
Stall Inception of Axial Fan with Foam Metal Casing Treatment	4
Computational Study on Fully Coupled Combustor–Turbine Interactions	4
Study of Boron Fuel in a Water-Breathing Ramjet	4
Performance of Water-Augmented Metallized Hybrid Propellant Ram Rocket During Underwater Motion	4
Parameter Influence on Porous Bleed Performance for Supersonic Turbulent Flows	4
Statistical Characterization of Emitter Fabrication over Electrospray Array Thruster	4
Experimental Investigation on Dilution of Disk-Shaped Pressure Gain Combustor Exhaust	4
Assessment of Pseudoshock Models Against Experiment in a Low-Aspect-Ratio Isolator	4
Evaluating the Effects of Fill Height in a Narrow Detonation Channel	4
Liquid Column Separation Due to Fluid Hammer Occurrence in Propellant Lines	4
Solid-Fuel Ramjet Regression Rate Measurements Using X-Ray Radiography and Ultrasonic Transducers	4
Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement	4
Microthrusters’ Combustion Control Using Jellied Propellant Flowing Through an Orifice Plate	4
Improving Detonability in a Small-Scale Rotating Detonation Engine Using Partial Premixing	4
Simultaneous CO and CO2 Laser Absorption Spectroscopy Sensing for Scramjet Combustion Characterization	4
Extinguishing and Combustion Characteristics of Electrically Controllable Solid Propellants Under Elevated Pressures	4
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor	4
Simulated Scramjet Shock Train Control Using an All-Coefficient Adaptive Control Approach	4
Performance Scaling of Modular Hybrid Propulsion System for Flight Vehicles	4
Numerical Analysis of a Novel Casing Treatment in an Axial Flow Fan	4
Ejector Recirculation and Entrainment	4
Processing and Testing Subscale Motors with Central Finocyl Grain Using Wax Mandrel	4
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions	4
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics	4
Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant	4
Electrospray Characteristics of High-Energetic Ionic Liquids: Ammonium Dinitramide and Hydroxyethylhydrazinium Nitrate	4
Flame-Spreading Process in Solid Rocket Motor with Fin Slots	4
Study on the Design Methodology of Turbine Profiles Operating Within Wide-Inflow-Angle Ranges	4
Seven-Zone Parametric Optimization Method for Compressor Profile with Controllable Maximum Thickness	4
Deflagration to Detonation Transition in Heterogeneous Mixtures Containing Ethanol/Acetone and Oxygen	3
Numerical Estimation of Nozzle Throat Heat Flux in Oxygen-Methane Rocket Engines	3
Reducing Preheating Requirements for 1-N-Scale Thruster with Ammonium Dinitramide-H2O2 Monopropellant	3
Similarity and Scaling in a Liquid-Fuel Ramjet Combustor	3
Optimized Postprocessing Method for Fatigue Life Evaluation of Reusable Rocket Combustion Chambers	3
Sloughing Prediction in Paraffin-Based Lattice-Augmented Hybrid Rocket Fuels	3
Effects of Thermal Expansion and Pressure on Far-Field Fluctuations of Heterogeneous Propellants	3
Methodology for Assessing Retrofitted Hydrogen Combustion and Fuel Cell Aircraft Environmental Impacts	3
Inlet Guide Vane Stagger Effects on Multistage Compressor Performance and Stall Inception	3
Propellant Surface Evolution of a Coaxial Pulsed Plasma Thruster	3
High-Pressure Combustion Characteristics of Hydroxyl-Terminated Polybutadiene Propellants	3
Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants	3
Lagrangian Simulation Methodology for Large-Eddy Simulations of Prefilming Air-Blast Injectors	3
Electrically Controlled Ignition Performance of LiClO4/PVA/H2O Propellants	3
Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine	3
Improving Base-Drag Corrections for Rotating Detonation Combustor Gross Thrust Measurements	3
Fuel Injector Requirements to Achieve Supercritical Flow at the Exit	3
Flow Characteristics in an Optically Accessible Solid Fuel Scramjet	2
Numerical Investigation of Super-Adiabatic Flame Temperature in Multislot Turbulent Premixed Hydrogen Flames	2
Modern Competing Flames Model for Composite Ammonium Perchlorate/Hydroxyl-Terminated Polybutadiene Propellant Combustion	2
Synchronized Initiation of Two Cylindrical Rotating Detonation Engines	2
Hypergolic Properties of Solvated Lithium, Sodium, and Calcium in Liquid Anhydrous Ammonia	2
Performance Impacts of Preheating the Primary Fuel Jet of an Ejector Ramjet	2
Automated Detection and Characterization of Aluminum Agglomerates in Solid Propellant Combustion	2
Computational Study of Propulsive Performance of Frozen Nano-Aluminum and Water (ALICE) Mixtures	2

Observation of Plasma Turbulence in a Hall Thruster Using Microwave Interferometry	2
Global Time-Resolved Measurements of Inlet/Isolator Unstart Induced by Mass Injection	2
Shear Coaxial Methane–Oxygen Injector Mixing and Combustion Examined by Laser Absorption Tomography	2
Effect of CO2 Dilution on Forced Ignition of Jet-A/Air Mixtures	2
Benefits of Spin Polarization for Inertial and Magneto-Inertial Fusion Propulsion	2
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet	2
Study of Suborbital Rocket Plane Using Highly Pressurized Hydrogen/Nitrous Oxide	2
Continuous Injector Geometry Variation to Augment Rotating Detonation Combustor Operation and Performance	2
Implicit Simulation of Turbomachinery Flows on Structured Meshes Using Graphics Processing Units	2
Multiple Diagnostics of Hybrid Rocket Ignition and Effect of Hypergolic Additive Granulometry	2
Announcements and Acknowledgements	2
Influence of Flight Conditions on the Combustion Characteristics of Solid-Fuel Ramjet	2
Tandem Energy-Analyzer/Mass-Spectrometer Measurements of an Ionic Liquid Ion Source	2
Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section	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 Nonuniform Plasma on Grid Erosion of the Water Ion Thruster	2
Effect of Boric Acid on Electronically Controlled Solid Propellants	2
Liquid Atomization in Rotary Slinger Injectors: Role of Liquid Delivery Manifold	2
Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes	2
Active Energy Management for Enhanced Engine Transient Operations	2
Demonstration of One Hundred Kilogram Xenon Throughput by a Low-Power Hall Thruster	2