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 2020-11-01 to 2024-11-01.)

Article	Citations
Numerical Analysis of Paraffin-Wax/Oxygen Hybrid Rocket Engines	24
Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine	22
Penetration and Combustion Studies of Tandem Liquid Jets in Supersonic Crossflow	14
Increased Thrust-to-Power Ratio of a Stepped-Diameter Helicon Plasma Thruster with Krypton Propellant	10
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine	10
Diode Laser Ignition Mechanism for Hybrid Propulsion Systems	10
Experimental Studies of Ice Crystal Accretion on Axisymmetric Bodies at Aeroengine Conditions	9
Statistics and Dynamics of Intermittent Boundary Layer Flashback in Swirl Flames	8
Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine	7
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics	7
Effects of Groove Structure on Spray Characteristics of a Throttleable Pintle Injector	7
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing	6
Flame Dynamics in an Optically Accessible Solid Fuel Ramjet Combustor	6
Decomposition of Ammonium-Perchlorate-Encapsulated Nanoscale and Micron-Scale Catalyst Particles	6
Regression and Flame Structure in Cavity Flameholding Solid-Fuel Ramjet Fuel Grains	6
Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence	5
Novel Hypergolic Green Fuels with Hydrogen Peroxide for Propulsion Systems	5
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor	5
Iodine Electric Propulsion System Thrust Validation: From Numerical Modeling to In-Space Testing	5
Flow Development in Radial Plane of Rotating Detonation Engine Integrated with Aerospike	5
Control of Large-Amplitude Combustion Oscillations Using Nanosecond Repetitively Pulsed Plasmas	5
Propellant Surface Evolution of a Coaxial Pulsed Plasma Thruster	4
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications	4
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet	4
Design of an Internal Osculating Waverider Intake	4

Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles	4
Role of Precombustion Chamber Design in Feed-System Coupled Instabilities of Hybrid Rockets	4
Simulated Scramjet Shock Train Control Using an All-Coefficient Adaptive Control Approach	4
Scramjet Engine Flowpath That Improves Specific Impulse Using JP-7 Fuel	4
Equivalent Supply Pressure for Pressure Gain Estimation in Rotating Detonation Engines	4
Rheological, Ballistic, and Mechanical Properties of 3D Printed, Photocured Composite Propellants	4
Uncertainty and Sensitivity Analysis of Bleed Modeling in Shock/Turbulent Interactions	3
Pulsed Electrogasdynamic Thruster for In-Space Propulsion	3
Ozone-Enhanced Flame Propagation of Methane/Ethylene/Air Mixtures at Subatmospheric Pressures	3
Increasing Burning Rate and Motor Thrust by Expandable Graphite Additives	3
Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants	3
Operation of a High-Power Nested Hall Thruster with Reduced Cathode Flow Fraction	3
Experimental Study on Infrared Radiation Characteristics and Matching Performance of Low-Observable Nozzles	3
Multiphase Effects on Solid Rocket Nozzle Performance	3
Impact of Design Constraints on Noise and Emissions of Derivative Supersonic Engines	3
Numerical Estimation of Nozzle Throat Heat Flux in Oxygen-Methane Rocket Engines	3
Optimal Design Algorithms for Bare Electrodynamic Tethers in the Active Mode	3
Nitrous Oxide Decomposition Using Inductively Heated Heat Exchangers	3
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	3
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability	2
Mechanisms Contributing to the Dynamic Stability of a Flexible Subscale Rocket Nozzle	2
Transient, Multiscale, Heterogeneous Model of Hydrogen Peroxide Decomposition for 3D-Printed Catalysts	2
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels	2
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet	2
Conceptual Design of a Space Power System Based on Combustion of Metals	2
Unsteady Stream-Tube Model for Pulse Performance of Bipropellant Thrusters	2
Analysis on Propulsive Performance of Hollow Rotating Detonation Engine with Laval Nozzle	2
Parameter Influence on Porous Bleed Performance for Supersonic Turbulent Flows	2
Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes	2
Numerical Performance Analysis of a Supersonic Combustor at Mach 8 Flight Off-Design Conditions	2
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets	2
Modern Competing Flames Model for Composite Ammonium Perchlorate/Hydroxyl-Terminated Polybutadiene Propellant Combustion	2
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions	2
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection	2
Observation of Plasma Turbulence in a Hall Thruster Using Microwave Interferometry	2
Performance Comparison of Paraffin/Ethanol Fuel Blends in a Laboratory-Scale Hybrid Rocket Motor	2
Optimization of Rotor Tip Cavity Shapes for Mitigating Aerodynamic Tip Leakage Losses	2
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor	2
Extinguishing and Combustion Characteristics of Electrically Controllable Solid Propellants Under Elevated Pressures	2
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype	1
Investigation of Unsteady Combustion Regimes in a Kerosene-Fueled Scramjet with Air Throttling	1
Bicyclo-HMX as an Energetic Additive for Composite Propellants	1
Computational Study on Fully Coupled Combustor–Turbine Interactions	1
Dynamic Regulation Process of the Variable-Geometry Power Turbine	1
Interaction Behavior of Pulsejet Engines	1
Novel Testing of a Water-Breathing Naval Ramjet at Underwater Cruise Conditions	1
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine	1
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests	1
Liquid Column Separation Due to Fluid Hammer Occurrence in Propellant Lines	1
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor	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
Low-Order Autoignition Modeling for Hydrogen Transverse Jets	1
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets	1
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing	1
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine	1
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters	1
Supersonic Combustion of Solid Fuels	1
Facility Effects on the Ion Characteristics of a 12.5-Kilowatt Hall Thruster	1
Aerodynamic Control of an Inlet Flow in Crosswind Using Peripheral Bleed Actuation	1
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge	1
Correction: Supercritical Mixing and Combustion of Liquid-Oxygen/Kerosene Bi-Swirl Injectors	1
Quasi-Two-Dimensional Simulation of a Rotating Detonation Engine Combustor and Injector	1
High-Current Density Performance of a Magnetically Shielded Hall Thruster	1
Liquid Atomization in Rotary Slinger Injectors: Role of Liquid Delivery Manifold	1
Critical Decay Time Model for Direct Detonation Initiation Energy in Gaseous Mixtures	1
Dynamic Machine Learning Global Optimization Algorithm and Its Application to Aerodynamics	1
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization	1
Aeroengine Stall Warning by Multicorrelation Analysis	1
Lagrangian Simulation Methodology for Large-Eddy Simulations of Prefilming Air-Blast Injectors	1