Journal of Propulsion and Power

Papers
(The median citation count of Journal of Propulsion and Power is 0. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2021-04-01 to 2025-04-01.)
ArticleCitations
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide17
Phenomenological Aerodynamic Analysis of an Ejector Exposed to Large Inlet Pulsations12
Chamber Length Limits of a Continuously Variable Geometry Rotating Detonation Combustor11
Thrust Vectoring of Double Divergent Nozzle Using Secondary Fluid Injection9
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels9
Shock-Stationary Application of Pseudoshock Models During High-Amplitude Combustion-Driven Unsteadiness9
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters8
Similarity and Scaling in a Liquid-Fuel Ramjet Combustor8
Announcements and Acknowledgements8
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines7
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy7
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver7
Novel Testing of a Water-Breathing Naval Ramjet at Underwater Cruise Conditions7
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine7
Effects of Groove Structure on Spray Characteristics of a Throttleable Pintle Injector6
Analysis of Transition to Thermo-Acoustic Instability in Swirl Combustor Using Variational Auto-Encoders6
Transitional Delayed Detached-Eddy Simulation for a Compressor Cascade: A Critical Assessment5
Investigation on Suppression of Hard-Start Phenomena in a Hypergolic Bipropellant Engine5
Increasing Burning Rate and Motor Thrust by Expandable Graphite Additives5
Multiphase Effects on Solid Rocket Nozzle Performance5
Scramjet Engine Flowpath That Improves Specific Impulse Using JP-7 Fuel5
Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes4
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant4
Improving Base-Drag Corrections for Rotating Detonation Combustor Gross Thrust Measurements4
Regression and Flame Structure in Cavity Flameholding Solid-Fuel Ramjet Fuel Grains4
Fuel Injector Requirements to Achieve Supercritical Flow at the Exit4
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization4
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation4
Transient, Multiscale, Heterogeneous Model of Hydrogen Peroxide Decomposition for 3D-Printed Catalysts4
Observation of Plasma Turbulence in a Hall Thruster Using Microwave Interferometry4
Performance Comparison of Paraffin/Ethanol Fuel Blends in a Laboratory-Scale Hybrid Rocket Motor4
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine4
Dynamic Machine Learning Global Optimization Algorithm and Its Application to Aerodynamics4
Propellant Surface Evolution of a Coaxial Pulsed Plasma Thruster3
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles3
Tandem Energy-Analyzer/Mass-Spectrometer Measurements of an Ionic Liquid Ion Source3
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing3
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake3
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants3
Hall Thruster System Using Dry Ice Propellant at the Triple Point3
Interaction Behavior of Pulsejet Engines3
Microthrusters’ Combustion Control Using Jellied Propellant Flowing Through an Orifice Plate3
Computational Study of Propulsive Performance of Frozen Nano-Aluminum and Water (ALICE) Mixtures3
Fuel Temperature Effects on Combustion Stability of a High-Pressure Liquid-Fueled Swirl Flame3
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine3
Flame Dynamics in an Optically Accessible Solid Fuel Ramjet Combustor3
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets3
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers3
Active Energy Management for Enhanced Engine Transient Operations3
Investigation of Intake Buzz Focusing on Shock Wave Movement and Inflow/Outflow Balance2
Hypersonic International Flight Research Experimentation Flight 2 Unstart Reliability Analysis2
Application of Boundary Layer Combustion in High-Mach-Number Scramjets2
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics2
Dynamics of a Centrifugally Confined Fusion Plasma in Space Propulsion Applications2
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan2
Liquid Atomization in Rotary Slinger Injectors: Role of Liquid Delivery Manifold2
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics2
Announcements and Acknowledgements2
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels2
Characterizing Hypergolic Propellants Using Impinging Jets and Droplets in Acoustic Levitation2
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection2
Parameter Influence on Porous Bleed Performance for Supersonic Turbulent Flows2
Announcements and Acknowledgments2
Analysis on Propulsive Performance of Hollow Rotating Detonation Engine with Laval Nozzle2
Mechanisms Contributing to the Dynamic Stability of a Flexible Subscale Rocket Nozzle1
Critical Decay Time Model for Direct Detonation Initiation Energy in Gaseous Mixtures1
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion1
Contrail Formation Criterion for Assessment of Alternative Propulsion Technologies1
Unsteady Stream-Tube Model for Pulse Performance of Bipropellant Thrusters1
Experimental Study on Infrared Radiation Characteristics and Matching Performance of Low-Observable Nozzles1
High-Current Density Performance of a Magnetically Shielded Hall Thruster1
Processing and Testing Subscale Motors with Central Finocyl Grain Using Wax Mandrel1
Statistical Characterization of Emitter Fabrication over Electrospray Array Thruster1
Effect of Boric Acid on Electronically Controlled Solid Propellants1
Review of Efficiency Losses for a Cooled Turbine Stage1
Performance of Water-Augmented Metallized Hybrid Propellant Ram Rocket During Underwater Motion1
Dynamic Regulation Process of the Variable-Geometry Power Turbine1
Iodine Electric Propulsion System Thrust Validation: From Numerical Modeling to In-Space Testing1
Bicyclo-HMX as an Energetic Additive for Composite Propellants1
Parametric Study of Corner Separation Control in a Compressor Cascade Using Endwall Blowing1
Delayed Detached-Eddy Simulations of Rough-Wall Turbulent Reactive Flows in a Supersonic Combustor1
Computational Study on Fully Coupled Combustor–Turbine Interactions1
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet1
Low-Order Autoignition Modeling for Hydrogen Transverse Jets1
Effect of Nonuniform Plasma on Grid Erosion of the Water Ion Thruster1
Scaling Laws at Stall in an Axial Compressor with an Upstream Perturbation1
Preparation, Ignition, and Combustion of Boron Fuels with CuO as an Additive1
Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology1
Flow Characteristics in an Optically Accessible Solid Fuel Scramjet1
Stochastic Emission in Passively Fed Single-Emitter Porous-Media Ionic Liquid Ion Sources1
Extinguishing and Combustion Characteristics of Electrically Controllable Solid Propellants Under Elevated Pressures1
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws1
Quasi-Two-Dimensional Simulation of a Rotating Detonation Engine Combustor and Injector1
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability1
Numerical Investigation of Diffusion Flame in Transonic Flow with Large Pressure Gradient1
Multiple Diagnostics of Hybrid Rocket Ignition and Effect of Hypergolic Additive Granulometry1
Solid-Fuel Ramjet Regression Rate Measurements Using X-Ray Radiography and Ultrasonic Transducers1
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations0
Effects of Thermal Expansion and Pressure on Far-Field Fluctuations of Heterogeneous Propellants0
Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition0
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests0
Secondary Combustion of Micron-Sized Magnesium Powder to Enhanced Kerosene-Fueled Scramjet Thrust0
Multipoint Aerodynamic Optimization of Three-Dimensional Ultra-High-Bypass-Ratio Engine Intakes0
Surface Structure of Reacting Solid Ramjet Fuels0
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power0
Supersonic Combustion of Solid Fuels0
Investigation of Gas-Turbine Afterburner with Aluminized Fuel-Rich Propellant0
Simulated Scramjet Shock Train Control Using an All-Coefficient Adaptive Control Approach0
Synchronized Initiation of Two Cylindrical Rotating Detonation Engines0
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor0
Modern Competing Flames Model for Composite Ammonium Perchlorate/Hydroxyl-Terminated Polybutadiene Propellant Combustion0
Liquid Oxygen/Gaseous Methane Single-Element Shear Coaxial Flame Dynamics0
Long-Duration Test of Coaxial Low-Energy Surface Flashover Ignitor0
Propagating an Electrospray Emission Model to Array Scales Using Particle-in-Cell0
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets0
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions0
Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment0
Aerodynamic Control of an Inlet Flow in Crosswind Using Peripheral Bleed Actuation0
Design of an Internal Osculating Waverider Intake0
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor0
Heat Release Rate from a Two-Phase Kerosene/Air Flame Using Chemiluminescence0
Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant0
Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine0
Methodology for Assessing Retrofitted Hydrogen Combustion and Fuel Cell Aircraft Environmental Impacts0
Acoustic Thrust Estimation on Turbofan Engines0
Effect of Ramp Geometry on Single Expansion Ramp Nozzle Performance Characteristics0
Experimental Investigation of Poly(methyl Methacrylate) Cooling Beds for Warm Gas Generator Applications0
Data-Driven Analysis of Tortuous Gas Turbine Inlet Truncation to Reduce Computational Cost0
Conceptual Design of a Space Power System Based on Combustion of Metals0
Inlet Guide Vane Stagger Effects on Multistage Compressor Performance and Stall Inception0
Effect of Fuel Injection Strategy on Generic Scramjet Combustor Operation0
Facility Effects on the Ion Characteristics of a 12.5-Kilowatt Hall Thruster0
Lagrangian Simulation Methodology for Large-Eddy Simulations of Prefilming Air-Blast Injectors0
Power Generation Characteristics of Disk-Shaped Magnetohydrodynamic Generator Driven by Rotating Detonation0
Shear Coaxial Methane–Oxygen Injector Mixing and Combustion Examined by Laser Absorption Tomography0
Benefits of Spin Polarization for Inertial and Magneto-Inertial Fusion Propulsion0
Numerical Simulation of Scram-Mode Operation of an Axisymmetric Combustor in an Arc Tunnel0
High-Voltage Discharge Optimization of a Hybrid-Wall Hall Thruster0
Effect of Accelerated Cyclic Aging on the Ballistic Properties of Composite Solid Propellant0
Continuous Injector Geometry Variation to Augment Rotating Detonation Combustor Operation and Performance0
Impact of Design Constraints on Noise and Emissions of Derivative Supersonic Engines0
Performance Evaluation of Damaged Blades Using Numerical Simulation and Machine Learning0
Rheological, Ballistic, and Mechanical Properties of 3D Printed, Photocured Composite Propellants0
Numerical Analysis of a Novel Casing Treatment in an Axial Flow Fan0
Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants0
Parametrical Investigation of Transverse Injection in a Dual-Bell Nozzle During Altitude-Varying Conditions0
Novel Hypergolic Green Fuels with Hydrogen Peroxide for Propulsion Systems0
Enhancing Hybrid Rocket Engine Regression Rates: The Stepped Helix Design0
Loss Mechanisms of Shrouded Stator Cavity Flow in an Axial Compressor0
Seven-Zone Parametric Optimization Method for Compressor Profile with Controllable Maximum Thickness0
Numerical Study on the Unsteady Behavior of the Solid-Fuel Scramjet0
A Refined Model to Predict Boundary of Instability of Axial Compressors0
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities0
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications0
Numerical Estimation of Nozzle Throat Heat Flux in Oxygen-Methane Rocket Engines0
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet0
Analytical Models for Time-Averaged Slit Flame Dynamics with Axial and Transverse Disturbances0
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates0
Optimization of Rotor Tip Cavity Shapes for Mitigating Aerodynamic Tip Leakage Losses0
Liquid Column Separation Due to Fluid Hammer Occurrence in Propellant Lines0
Noise Reduction of Distributed Propulsion by Optimized Phase Synchronization0
Deflagration to Detonation Transition in Heterogeneous Mixtures Containing Ethanol/Acetone and Oxygen0
Current Status of Liquid-Bipropellant Detonation-Based Propulsion Devices0
Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence0
Equivalent Supply Pressure for Pressure Gain Estimation in Rotating Detonation Engines0
Hybrid Modeling of Miniaturized 50 W Annular Hall Thruster0
Reducing Preheating Requirements for 1-N-Scale Thruster with Ammonium Dinitramide-H2O2 Monopropellant0
Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking0
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype0
Aeroengine Stall Warning by Multicorrelation Analysis0
Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section0
Control of Large-Amplitude Combustion Oscillations Using Nanosecond Repetitively Pulsed Plasmas0
Optimization of Thrust of a Generic X-51 Hypersonic Vehicle0
Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine0
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet0
General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants0
Optimal Design Algorithms for Bare Electrodynamic Tethers in the Active Mode0
Optimal Liquid Engine Architecture by Performance-Cooling Tradeoff Analysis0
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge0
Investigation of Unsteady Combustion Regimes in a Kerosene-Fueled Scramjet with Air Throttling0
Free-Windmilling Speed Prediction Based on Aerodynamic Similarity of an Axial Wide-Chord Fan0
Performance Scaling of Modular Hybrid Propulsion System for Flight Vehicles0
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor0
Flow Development in Radial Plane of Rotating Detonation Engine Integrated with Aerospike0
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator0
Assessment of Pseudoshock Models Against Experiment in a Low-Aspect-Ratio Isolator0
Uncertainty and Sensitivity Analysis of Bleed Modeling in Shock/Turbulent Interactions0
Optimization and Testing of DC Electromagnetic Pump for Liquid Metal Space Use0
Simplified Data-Reduction Method for Hybrid Propulsion0
Monodisperse Porous Emitter Materials for Ion Electrospray Propulsion0
Beam Misalignment Effects on Microwave Rocket Propulsion Performance0
Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles0
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor0
Brayton Cycle Analysis of the Effect of Wake Ingestion on Aircraft Range0
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