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 2020-05-01 to 2024-05-01.)

Article	Citations
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
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview	12
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	7
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 study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel	6
Investigation of Flow Distortion Generated Forced Response of a Radial Turbine with Vaneless Volute	4
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration	4
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage	3
Predicting remaining useful life of turbofan engines using degradation signal based echo state network	3
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber	3
One-equation turbulence models applied to practical scramjet inlet	3
Large-Eddy Simulation of Shaped Hole Film Cooling with the Influence of Cross Flow	3
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor	3
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach	3
Film Cooling Experimental Study on Sinusoidal Corrugated Liner for Afterburner	3
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system	2
A new method to improve the real-time performance of aero-engine component level model	2
Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel	2
Study on Influence of Diameter on Detonation Acoustic Characteristics of Pulse Detonation Engine	2
Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel	2
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter	2
Effect of multi-hole arrangement on the effusion cooling with backward injection	2

Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario	2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions	2
Control of subsonic jets using vanes as vortex generators	2
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients	2
Modal Analysis of the Axial Compressor Blade: Advanced Time-Dependent Electronic Interferometry and Finite Element Method	2
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment	2
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients	2
Experimental research on the performance of the forward variable area bypass injector for variable cycle engines	2
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor	2
A Study on the Effect of Angle in Diffused Hole Film Cooling Effectiveness at Different Blowing Ratios	2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions	2
Modeling and mode transition simulation of over-under turbine based combined cycle (TBCC) propulsion system based on inlet/engine matching	2
Active fault tolerant control of turbofan engines with actuator faults under disturbances	1
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine	1
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser	1
Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature	1
An improved compact propulsion system model based on batch normalize deep neural network	1
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper	1
Supersonic jet mixing in the presence of two annular co-flow streams	1
Combined Flow Control of Positively Bowed Blade and Vortex Generator Jet on a Compressor Cascade	1
Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor	1
Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils	1
Modeling and analysis of 3D radiative heat transfer in combustor	1
Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model	1
Numerical analysis of high temperature gas flow through conical micronozzle	1
Optimization of a circumferential groove in a centrifugal compressor	1
Experimental research on the performance of the forward variable area bypass injector for variable cycle engines	1
Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins	1
Modeling and validation of the volume effect on the axial fan transient performance	1
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine	1
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence	1
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates	1
Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application	1
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine	1
Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex	1
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine	1
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions	1
Characterization of titanium grade 5 alloy compressor blade in a jet engine using advanced materials for optimum thrust production	1
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview	1
Research on the influence of honeycomb cell blockage on the seal leakage characteristics	1
Conjugate heat transfer analysis of a radially cooled nozzle guide vane in an aero gas turbine engine	1
Numerical Investigation on the Cold Flow Field of a Typical Cavity-based Scramjet Combustor with Double Ramp Entry	1
Influence of nozzle exit geometrical parameters on supersonic jet decay	1
Influence of innovative hydrogen multi strut injector with different spacing on cavity-based scramjet combustor	1
The influence of the geometry of V-gutter bluff body on transient vortex shedding	1
Research on a high-precision real-time improvement method for aero-engine component-level model	1
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis	1
Active fault tolerant control of turbofan engines with actuator faults under disturbances	1
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications	1
Control-oriented quasi-one dimensional modeling method for scramjet	1

An active fault-tolerant control strategy of aircraft engines based on multi-model predictive control	1
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper	1
Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application	1
Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor	1
Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation	1
Optimization of ACE mode transition control schedule considering geometric adjustment speed	1
A new method to improve the real-time performance of aero-engine component level model	1
Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade	1
A new compilation method of general standard test load spectrum for aircraft engine	1
A study on design optimization for compressor blisks	1
Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model	1
Large Eddy Simulation of Secondary Flows in an Ultra-High Lift Low Pressure Turbine Cascade at Various Inlet Incidences	1