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 2021-06-01 to 2025-06-01.)

Article	Citations
Announcements and Acknowledgements	17
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy	14
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant	13
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization	13
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	11
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
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
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet	6
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
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor	5

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
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
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
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
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