OOIR: Observatory of International Research

Papers

(The TQCC of Journal of Propulsion and Power is 3. 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 2021-08-01 to 2025-08-01.)

Article	Citations
Announcements and Acknowledgements	17
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy	16
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant	15
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization	14
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine	13
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver	12
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	11
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics	11
Correlation for Restart Boundaries of Simplified Two-Dimensional Hypersonic Inlets	11
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels	10
Dynamic Regulation Process of the Variable-Geometry Power Turbine	10
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers	10
Preparation, Ignition, and Combustion of Boron Fuels with CuO as an Additive	9
Characterizing Hypergolic Propellants Using Impinging Jets and Droplets in Acoustic Levitation	9
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
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion	8
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge	7
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor	7
Loss Mechanisms of Shrouded Stator Cavity Flow in an Axial Compressor	7
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet	7
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets	7
General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants	7
Data-Driven Wall Pressure Reconstruction and Sparse Sensor Optimization for Supersonic Nozzles	7

Effect of Fuel Injection Strategy on Generic Scramjet Combustor Operation	6
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests	6
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor	6
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities	6
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet	5
Surface Structure of Reacting Solid Ramjet Fuels	5
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation	5
Multipoint Aerodynamic Optimization of Three-Dimensional Ultra-High-Bypass-Ratio Engine Intakes	5
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels	5
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide	5
Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles	5
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor	5
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles	5
Interaction Behavior of Pulsejet Engines	4
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets	4
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations	4
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing	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
Low-Order Autoignition Modeling for Hydrogen Transverse Jets	4
Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets Using LOX	4
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants	4
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan	4
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake	4
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws	4
Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking	3
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates	3
Design of an Internal Osculating Waverider Intake	3
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine	3
Hall Thruster System Using Dry Ice Propellant at the Triple Point	3
Performance of Water-Augmented Metallized Hybrid Propellant Ram Rocket During Underwater Motion	3
Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition	3
Data-Driven Analysis of Tortuous Gas Turbine Inlet Truncation to Reduce Computational Cost	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
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications	3
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters	3
Microthrusters’ Combustion Control Using Jellied Propellant Flowing Through an Orifice Plate	3
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics	3
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power	3
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype	3
Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine	3
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator	3
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine	3
Announcements and Acknowledgments	3
Development and Evaluation of Reduced Kinetics Models for 1,3-Butadiene–Air Combustion	3
Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment	3