OOIR: Observatory of International Research

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 2020-03-01 to 2024-03-01.)

Article	Citations
Numerical Analysis of Paraffin-Wax/Oxygen Hybrid Rocket Engines	23
Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine	16
Penetration and Combustion Studies of Tandem Liquid Jets in Supersonic Crossflow	11
Increased Thrust-to-Power Ratio of a Stepped-Diameter Helicon Plasma Thruster with Krypton Propellant	10
Statistics and Dynamics of Intermittent Boundary Layer Flashback in Swirl Flames	8
Experimental Studies of Ice Crystal Accretion on Axisymmetric Bodies at Aeroengine Conditions	8
Diode Laser Ignition Mechanism for Hybrid Propulsion Systems	6
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine	6
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing	5
Flame Dynamics in an Optically Accessible Solid Fuel Ramjet Combustor	5
Control of Large-Amplitude Combustion Oscillations Using Nanosecond Repetitively Pulsed Plasmas	5
Effects of Groove Structure on Spray Characteristics of a Throttleable Pintle Injector	5
Equivalent Supply Pressure for Pressure Gain Estimation in Rotating Detonation Engines	4
Role of Precombustion Chamber Design in Feed-System Coupled Instabilities of Hybrid Rockets	4
Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine	4
Decomposition of Ammonium-Perchlorate-Encapsulated Nanoscale and Micron-Scale Catalyst Particles	4
Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence	3
Design of an Internal Osculating Waverider Intake	3
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics	3
Operation of a High-Power Nested Hall Thruster with Reduced Cathode Flow Fraction	3
Simulated Scramjet Shock Train Control Using an All-Coefficient Adaptive Control Approach	3
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	3
Pulsed Electrogasdynamic Thruster for In-Space Propulsion	3
Ozone-Enhanced Flame Propagation of Methane/Ethylene/Air Mixtures at Subatmospheric Pressures	3
Scramjet Engine Flowpath That Improves Specific Impulse Using JP-7 Fuel	2

Numerical Estimation of Nozzle Throat Heat Flux in Oxygen-Methane Rocket Engines	2
Iodine Electric Propulsion System Thrust Validation: From Numerical Modeling to In-Space Testing	2
Transient, Multiscale, Heterogeneous Model of Hydrogen Peroxide Decomposition for 3D-Printed Catalysts	2
Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes	2
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor	2
Rheological, Ballistic, and Mechanical Properties of 3D Printed, Photocured Composite Propellants	2
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions	2
Propellant Surface Evolution of a Coaxial Pulsed Plasma Thruster	2
Numerical Performance Analysis of a Supersonic Combustor at Mach 8 Flight Off-Design Conditions	2
Uncertainty and Sensitivity Analysis of Bleed Modeling in Shock/Turbulent Interactions	2
Conceptual Design of a Space Power System Based on Combustion of Metals	2
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles	2
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet	1
Bicyclo-HMX as an Energetic Additive for Composite Propellants	1
Unsteady Stream-Tube Model for Pulse Performance of Bipropellant Thrusters	1
Quasi-Two-Dimensional Simulation of a Rotating Detonation Engine Combustor and Injector	1
Parameter Influence on Porous Bleed Performance for Supersonic Turbulent Flows	1
Increasing Burning Rate and Motor Thrust by Expandable Graphite Additives	1
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization	1
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels	1
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications	1
Lagrangian Simulation Methodology for Large-Eddy Simulations of Prefilming Air-Blast Injectors	1
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor	1
Correction: Supercritical Mixing and Combustion of Liquid-Oxygen/Kerosene Bi-Swirl Injectors	1
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion	1
Solid-Fuel Ramjet Regression Rate Measurements Using X-Ray Radiography and Ultrasonic Transducers	1
Critical Decay Time Model for Direct Detonation Initiation Energy in Gaseous Mixtures	1
Nitrous Oxide Decomposition Using Inductively Heated Heat Exchangers	1
Observation of Plasma Turbulence in a Hall Thruster Using Microwave Interferometry	1
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters	1
Impact of Design Constraints on Noise and Emissions of Derivative Supersonic Engines	1
Facility Effects on the Ion Characteristics of a 12.5-Kilowatt Hall Thruster	1
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge	1
Optimal Design Algorithms for Bare Electrodynamic Tethers in the Active Mode	1
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability	1
Low-Order Autoignition Modeling for Hydrogen Transverse Jets	1
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection	1
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing	1
Novel Testing of a Water-Breathing Naval Ramjet at Underwater Cruise Conditions	1
Regression and Flame Structure in Cavity Flameholding Solid-Fuel Ramjet Fuel Grains	1
Flow Development in Radial Plane of Rotating Detonation Engine Integrated with Aerospike	1
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor	1
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets	0
Liquid Column Separation Due to Fluid Hammer Occurrence in Propellant Lines	0
Announcements and Acknowledgments	0
Modern Competing Flames Model for Composite Ammonium Perchlorate/Hydroxyl-Terminated Polybutadiene Propellant Combustion	0
Interaction Behavior of Pulsejet Engines	0
Optimization of Rotor Tip Cavity Shapes for Mitigating Aerodynamic Tip Leakage Losses	0
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet	0
Hypersonic International Flight Research Experimentation Flight 2 Unstart Reliability Analysis	0

Effect of Accelerated Cyclic Aging on the Ballistic Properties of Composite Solid Propellant	0
Novel Hypergolic Green Fuels with Hydrogen Peroxide for Propulsion Systems	0
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine	0
Correction: An Algebraic Model for Structural and Life Analysis of Regeneratively-Cooled Thrust Chambers	0
Correction: Physical Insight into Fuel-Air Mixing for Upstream-Fuel-Injected Scramjets via Multi-Objective Design Optimization	0
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver	0
Deflagration to Detonation Transition in Heterogeneous Mixtures Containing Ethanol/Acetone and Oxygen	0
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine	0
Surface Structure of Reacting Solid Ramjet Fuels	0
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics	0
Dynamic Machine Learning Global Optimization Algorithm and Its Application to Aerodynamics	0
Performance Evaluation of Damaged Blades Using Numerical Simulation and Machine Learning	0
Simplified Data-Reduction Method for Hybrid Propulsion	0
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates	0
Parametrical Investigation of Transverse Injection in a Dual-Bell Nozzle During Altitude-Varying Conditions	0
Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant	0
Acoustic Thrust Estimation on Turbofan Engines	0
Dynamic Regulation Process of the Variable-Geometry Power Turbine	0
Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology	0
Analysis on Propulsive Performance of Hollow Rotating Detonation Engine with Laval Nozzle	0
Long-Duration Test of Coaxial Low-Energy Surface Flashover Ignitor	0
Computational Study on Fully Coupled Combustor–Turbine Interactions	0
Transitional Delayed Detached-Eddy Simulation for a Compressor Cascade: A Critical Assessment	0
Free-Windmilling Speed Prediction Based on Aerodynamic Similarity of an Axial Wide-Chord Fan	0
Extinguishing and Combustion Characteristics of Electrically Controllable Solid Propellants Under Elevated Pressures	0
Fuel Injector Requirements to Achieve Supercritical Flow at the Exit	0
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power	0
Liquid Atomization in Rotary Slinger Injectors: Role of Liquid Delivery Manifold	0
Performance Comparison of Paraffin/Ethanol Fuel Blends in a Laboratory-Scale Hybrid Rocket Motor	0
Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section	0
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant	0
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests	0
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan	0
Multiphase Effects on Solid Rocket Nozzle Performance	0
Heat Release Rate from a Two-Phase Kerosene/Air Flame Using Chemiluminescence	0
Aerodynamic Control of an Inlet Flow in Crosswind Using Peripheral Bleed Actuation	0
Beam Misalignment Effects on Microwave Rocket Propulsion Performance	0
Continuous Injector Geometry Variation to Augment Rotating Detonation Combustor Operation and Performance	0
Experimental Investigation of Poly(methyl Methacrylate) Cooling Beds for Warm Gas Generator Applications	0
Assessment of Pseudoshock Models Against Experiment in a Low-Aspect-Ratio Isolator	0
Microthrusters’ Combustion Control Using Jellied Propellant Flowing Through an Orifice Plate	0
Numerical Investigation of Diffusion Flame in Transonic Flow with Large Pressure Gradient	0
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels	0
Aeroengine Stall Warning by Multicorrelation Analysis	0
Correction: Fundamental Scramjet Combustion Experiments Using Hydrocarbon Fuel	0
Announcements and Acknowledgements	0
Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment	0
Liquid Oxygen/Gaseous Methane Single-Element Shear Coaxial Flame Dynamics	0
Analysis of Transition to Thermo-Acoustic Instability in Swirl Combustor Using Variational Auto-Encoders	0
Benefits of Spin Polarization for Inertial and Magneto-Inertial Fusion Propulsion	0
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy	0
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet	0
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets	0
Similarity and Scaling in a Liquid-Fuel Ramjet Combustor	0
Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants	0
Mechanisms Contributing to the Dynamic Stability of a Flexible Subscale Rocket Nozzle	0
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator	0
Correction: Effects of Water Vapor Propellant on Electrodeless Thruster Performance	0
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype	0
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities	0