OOIR: Observatory of International Research

Papers

(The median citation count of Journal of Propulsion and Power is 1. 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 2021-06-01 to 2025-06-01.)

Article	Citations
Announcements and Acknowledgements	17
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy	14
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization	13
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant	13
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver	11
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics	11
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine	11
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	11
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels	10
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers	9
Dynamic Regulation Process of the Variable-Geometry Power Turbine	9
Characterizing Hypergolic Propellants Using Impinging Jets and Droplets in Acoustic Levitation	9
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion	8
Preparation, Ignition, and Combustion of Boron Fuels with CuO as an Additive	8
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability	8
Stochastic Emission in Passively Fed Single-Emitter Porous-Media Ionic Liquid Ion Sources	8
Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology	8
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor	7
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets	7
General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants	7
Loss Mechanisms of Shrouded Stator Cavity Flow in an Axial Compressor	7
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities	6
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge	6
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet	6
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests	5

Surface Structure of Reacting Solid Ramjet Fuels	5
Effect of Fuel Injection Strategy on Generic Scramjet Combustor Operation	5
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet	5
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor	5
Multipoint Aerodynamic Optimization of Three-Dimensional Ultra-High-Bypass-Ratio Engine Intakes	4
Injection Temperature and Scheme Effects on Neutral Flow Dynamics in Hall Thrusters	4
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection	4
Interaction Behavior of Pulsejet Engines	4
Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles	4
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation	4
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide	4
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan	4
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor	4
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels	4
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants	4
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles	4
Design of an Internal Osculating Waverider Intake	3
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator	3
Data-Driven Analysis of Tortuous Gas Turbine Inlet Truncation to Reduce Computational Cost	3
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications	3
Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets Using LOX	3
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing	3
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype	3
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates	3
Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking	3
Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment	3
Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition	3
Low-Order Autoignition Modeling for Hydrogen Transverse Jets	3
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake	3
Delayed Detached-Eddy Simulations of Rough-Wall Turbulent Reactive Flows in a Supersonic Combustor	3
Beam Misalignment Effects on Microwave Rocket Propulsion Performance	3
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power	3
Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine	3
Hall Thruster System Using Dry Ice Propellant at the Triple Point	3
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws	3
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations	3
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets	3
Parameter Influence on Porous Bleed Performance for Supersonic Turbulent Flows	2
Announcements and Acknowledgments	2
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine	2
Extinguishing and Combustion Characteristics of Electrically Controllable Solid Propellants Under Elevated Pressures	2
Statistical Characterization of Emitter Fabrication over Electrospray Array Thruster	2
Numerical Analysis of a Novel Casing Treatment in an Axial Flow Fan	2
Evaluating the Effects of Fill Height in a Narrow Detonation Channel	2
Development and Evaluation of Reduced Kinetics Models for 1,3-Butadiene–Air Combustion	2
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters	2
Computational Study on Fully Coupled Combustor–Turbine Interactions	2
Processing and Testing Subscale Motors with Central Finocyl Grain Using Wax Mandrel	2
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions	2
Simulated Scramjet Shock Train Control Using an All-Coefficient Adaptive Control Approach	2

Ejector Recirculation and Entrainment	2
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics	2
Performance of Water-Augmented Metallized Hybrid Propellant Ram Rocket During Underwater Motion	2
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine	2
Microthrusters’ Combustion Control Using Jellied Propellant Flowing Through an Orifice Plate	2
Solid-Fuel Ramjet Regression Rate Measurements Using X-Ray Radiography and Ultrasonic Transducers	2
Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement	2
Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant	2
Improving Base-Drag Corrections for Rotating Detonation Combustor Gross Thrust Measurements	1
Numerical Estimation of Nozzle Throat Heat Flux in Oxygen-Methane Rocket Engines	1
Electrically Controlled Ignition Performance of LiClO₄/PVA/H₂O Propellants	1
Liquid Column Separation Due to Fluid Hammer Occurrence in Propellant Lines	1
Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants	1
Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes	1
Continuous Injector Geometry Variation to Augment Rotating Detonation Combustor Operation and Performance	1
Flow Characteristics in an Optically Accessible Solid Fuel Scramjet	1
Novel Hypergolic Green Fuels with Hydrogen Peroxide for Propulsion Systems	1
Announcements and Acknowledgements	1
Reducing Preheating Requirements for 1-N-Scale Thruster with Ammonium Dinitramide-H2O2 Monopropellant	1
Effect of Boric Acid on Electronically Controlled Solid Propellants	1
Methodology for Assessing Retrofitted Hydrogen Combustion and Fuel Cell Aircraft Environmental Impacts	1
Liquid Atomization in Rotary Slinger Injectors: Role of Liquid Delivery Manifold	1
Performance Scaling of Modular Hybrid Propulsion System for Flight Vehicles	1
Seven-Zone Parametric Optimization Method for Compressor Profile with Controllable Maximum Thickness	1
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor	1
Observation of Plasma Turbulence in a Hall Thruster Using Microwave Interferometry	1
Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section	1
Synchronized Initiation of Two Cylindrical Rotating Detonation Engines	1
Effect of Nonuniform Plasma on Grid Erosion of the Water Ion Thruster	1
Active Energy Management for Enhanced Engine Transient Operations	1
Similarity and Scaling in a Liquid-Fuel Ramjet Combustor	1
Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine	1
Tandem Energy-Analyzer/Mass-Spectrometer Measurements of an Ionic Liquid Ion Source	1
Deflagration to Detonation Transition in Heterogeneous Mixtures Containing Ethanol/Acetone and Oxygen	1
Lagrangian Simulation Methodology for Large-Eddy Simulations of Prefilming Air-Blast Injectors	1
Assessment of Pseudoshock Models Against Experiment in a Low-Aspect-Ratio Isolator	1
Propellant Surface Evolution of a Coaxial Pulsed Plasma Thruster	1
Fuel Injector Requirements to Achieve Supercritical Flow at the Exit	1
Modern Competing Flames Model for Composite Ammonium Perchlorate/Hydroxyl-Terminated Polybutadiene Propellant Combustion	1
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet	1
Influence of Flight Conditions on the Combustion Characteristics of Solid-Fuel Ramjet	1
Computational Study of Propulsive Performance of Frozen Nano-Aluminum and Water (ALICE) Mixtures	1
Inlet Guide Vane Stagger Effects on Multistage Compressor Performance and Stall Inception	1
Multiple Diagnostics of Hybrid Rocket Ignition and Effect of Hypergolic Additive Granulometry	1
Effects of Thermal Expansion and Pressure on Far-Field Fluctuations of Heterogeneous Propellants	1