OOIR: Observatory of International Research

Papers

(The TQCC of International Journal of Turbo & Jet-Engines 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 2020-03-01 to 2024-03-01.)

Article	Citations
The Effect of TiO2 on Engine Emissions for Gas Turbine engine Fueled with jatropha, butanol, Soya and Rapeseed Oil	27
Exergetic, Exergoeconomic, Sustainability and Environmental Damage Cost Analyses of J85 Turbojet Engine with Afterburner	26
Fatigue Life Prediction of Fan Blade Using Nominal Stress Method and Cumulative Fatigue Damage Theory	18
Effect of Primary Rocket Jet on Thermodynamic Cycle of RBCC in Ejector Mode	11
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview	10
Exergy analysis of a turboprop engine at different flight altitude and speeds using novel consideration	8
Design and Numerical Investigations on a Dual-Duct Variable Geometry RBCC Inlet	6
Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel	6
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser	6
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine	6
Numerical Prediction of 45° Angled Ribs Effects on U-shaped Channels Heat Transfer and Flow under Multi Conditions	5
Study on Acoustic Detection of the Working State of Pulse Detonation Engine	5
The Relationship of Spike Stall and Hub Corner Separation in Axial Compressor	4
Investigation of Flow Distortion Generated Forced Response of a Radial Turbine with Vaneless Volute	4
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach	3
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration	3
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor	3
One-equation turbulence models applied to practical scramjet inlet	3
Dynamic Characteristics Analysis and Optimization Design of a Simulated Power Turbine Rotor Based on Finite Element Method	3
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage	3
Film Cooling Experimental Study on Sinusoidal Corrugated Liner for Afterburner	3
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber	3
Modeling and mode transition simulation of over-under turbine based combined cycle (TBCC) propulsion system based on inlet/engine matching	2
Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario	2
Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel	2

Predicting remaining useful life of turbofan engines using degradation signal based echo state network	2
Study on Influence of Diameter on Detonation Acoustic Characteristics of Pulse Detonation Engine	2
Modal Analysis of the Axial Compressor Blade: Advanced Time-Dependent Electronic Interferometry and Finite Element Method	2
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter	2
A Research on Aero-engine Control Based on Deep Q Learning	2
Aeroengine Performance Prediction Based on Double-Extremum Learning Particle Swarm Optimization	2
A new method to improve the real-time performance of aero-engine component level model	2
Control of subsonic jets using vanes as vortex generators	2
Large-Eddy Simulation of Shaped Hole Film Cooling with the Influence of Cross Flow	2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions	2
Effect of multi-hole arrangement on the effusion cooling with backward injection	2
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients	2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions	2
Experimental research on the performance of the forward variable area bypass injector for variable cycle engines	2
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients	2
A Study on the Effect of Angle in Diffused Hole Film Cooling Effectiveness at Different Blowing Ratios	2
Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade	1
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system	1
Characterization of titanium grade 5 alloy compressor blade in a jet engine using advanced materials for optimum thrust production	1
Optimization of a circumferential groove in a centrifugal compressor	1
Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model	1
Active fault tolerant control of turbofan engines with actuator faults under disturbances	1
Conjugate heat transfer analysis of a radially cooled nozzle guide vane in an aero gas turbine engine	1
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis	1
Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature	1
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates	1
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine	1
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine	1
Research on Nozzle Jet Vector Control with Synthetic Jet Technology	1
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper	1
Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel	1
Modeling and analysis of 3D radiative heat transfer in combustor	1
Numerical analysis of high temperature gas flow through conical micronozzle	1
A new compilation method of general standard test load spectrum for aircraft engine	1
Experimental research on the performance of the forward variable area bypass injector for variable cycle engines	1
Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model	1
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber	1
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment	1
Large Eddy Simulation of Secondary Flows in an Ultra-High Lift Low Pressure Turbine Cascade at Various Inlet Incidences	1
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine	1
Modeling and validation of the volume effect on the axial fan transient performance	1
Blade Number Selection for a Splittered Mixed-Flow Compressor Impeller Using Improved Loss Model	1
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper	1
An improved compact propulsion system model based on batch normalize deep neural network	1
An active fault-tolerant control strategy of aircraft engines based on multi-model predictive control	1
Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor	1
Research on the influence of honeycomb cell blockage on the seal leakage characteristics	1
Optimization of ACE mode transition control schedule considering geometric adjustment speed	1
Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation	1
Influence of nozzle exit geometrical parameters on supersonic jet decay	1

A new method to improve the real-time performance of aero-engine component level model	1
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications	1
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine	1
Research on a high-precision real-time improvement method for aero-engine component-level model	1
The influence of the geometry of V-gutter bluff body on transient vortex shedding	1
Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application	1
Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex	1
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor	1
Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application	1
Combined Flow Control of Positively Bowed Blade and Vortex Generator Jet on a Compressor Cascade	1
Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor	1