Journal of Propulsion and Power

Papers
(The TQCC of Journal of Propulsion and Power is 5. 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 2022-06-01 to 2026-06-01.)
ArticleCitations
Announcements and Acknowledgements32
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy32
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant29
Expandable Graphite, a Novel Regression Rate Enhancer in the Solid Fuel Ramjet26
Correlation for Restart Boundaries of Simplified Two-Dimensional Hypersonic Inlets26
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver25
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine23
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization19
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines19
Experimental Comparison of Jet Modes Using Self-Excited Sweeping Jet Actuator in Compressor Cascades19
Preparation, Ignition, and Combustion of Boron Fuels with CuO as an Additive18
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics18
Combustion of 3D Printable Hybrid Rocket Fuels17
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels16
Characterizing Hypergolic Propellants Using Impinging Jets and Droplets in Acoustic Levitation16
Firing Tests and Simulations of a CubeSat-Scale H2O2-Based Hybrid Rocket15
Simulation of Vacuum Chamber Pressure Distributions with Uncertainty Quantification15
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers14
Dynamic Regulation Process of the Variable-Geometry Power Turbine14
Structure and Stabilization Mechanisms of an Ethylene Flame in Supersonic Coflow14
Stochastic Emission in Passively Fed Single-Emitter Porous-Media Ionic Liquid Ion Sources13
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability13
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion13
Improved Response Function for Low-Order Modeling of Longitudinal Combustion Instabilities13
Loss Mechanisms of Shrouded Stator Cavity Flow in an Axial Compressor12
Data-Driven Wall Pressure Reconstruction and Sparse Sensor Optimization for Supersonic Nozzles12
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor12
Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology12
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities12
Effect of Varying Secondary Swirl Injector Location on Performance of Hybrid Rocket12
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet11
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet11
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge11
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets11
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor11
General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants11
Effect of Fuel Injection Strategy on Generic Scramjet Combustor Operation11
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests10
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor9
Pilot Injection Impact on Ignition of F-24/ATJ Blends Under Various Conditions9
Multipoint Aerodynamic Optimization of Three-Dimensional Ultra-High-Bypass-Ratio Engine Intakes9
Thermal and Resonance Characteristics of Tapered Cavities of Various Lengths9
Performance of Novel Electrode Structures for Electrically Controlled Solid Propellant9
Surface Structure of Reacting Solid Ramjet Fuels9
Combustion of Preheated Hydrocarbon Fuel in a Scramjet Model Combustor9
Uncertainty Quantification of Slab Burner Simulation: Surrogates, Forward Propagation, and Parameter Calibration8
Characterization of a Nanonewton-Sensitivity Counterbalanced Pendulum Thrust Stand for Pulsed Propulsion Systems8
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels8
Effects of Evaporation Modeling on Kerosene–Air Oblique Detonation8
Evaluation of Radiative Heat-Transfer Effect on Paraffin-Wax Regression Rate in Hybrid Rocket8
Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles8
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide8
Injection Temperature and Scheme Effects on Neutral Flow Dynamics in Hall Thrusters7
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles7
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection7
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants7
Erosion Mechanisms of Baffle Plates at Stagnation Point in Hybrid Rockets7
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing7
Supersonic Combustion and Flow Evolution in Dual-Combustion Ramjet Engine7
Reducing Aluminum Agglomeration in Composite Propellants with Gallium and Indium Additives7
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation7
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake7
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan7
Interaction Behavior of Pulsejet Engines6
Delayed Detached-Eddy Simulations of Rough-Wall Turbulent Reactive Flows in a Supersonic Combustor6
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws6
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets6
Low-Order Autoignition Modeling for Hydrogen Transverse Jets6
Unraveling the Transition from Standard to Reactive Atomization of Hypergolic Propellants6
Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets Using LOX6
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations6
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype5
Data-Driven Analysis of Tortuous Gas Turbine Inlet Truncation to Reduce Computational Cost5
Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine5
Performance Test of a Diode Laser-Sustained Plasma Thruster Using Argon5
Characterizing the Oscillatory Unstart/Restart of a Supersonic Stator in Unsteady Conditions5
Control of Shock-Induced Flow Separation Using Rectangular Air-Jet Vortex Generators5
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator5
High-Specific-Impulse Electrospray Propulsion with Small Capillary Emitters5
Flame Structures in a Model Solid Fuel Ramjet with Increasing Reynolds Numbers5
Design of an Internal Osculating Waverider Intake5
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power5
Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking5
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates5
Beam Misalignment Effects on Microwave Rocket Propulsion Performance5
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