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 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
Diode Laser Ignition Mechanism for Hybrid Propulsion Systems	10
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
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
Effects of Groove Structure on Spray Characteristics of a Throttleable Pintle Injector	7
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
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
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing	6
Flame Dynamics in an Optically Accessible Solid Fuel Ramjet Combustor	6
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
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
Equivalent Supply Pressure for Pressure Gain Estimation in Rotating Detonation Engines	4
Rheological, Ballistic, and Mechanical Properties of 3D Printed, Photocured Composite Propellants	4
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
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
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