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

Article	Citations
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview	11
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration	7
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview	6
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine	6
Predicting remaining useful life of turbofan engines using degradation signal based echo state network	5
Modeling and mode transition simulation of over-under turbine based combined cycle (TBCC) propulsion system based on inlet/engine matching	5
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage	4
One-equation turbulence models applied to practical scramjet inlet	4
Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel	4
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach	3
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients	3
A study on design optimization for compressor blisks	3
Effect of multi-hole arrangement on the effusion cooling with backward injection	3
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system	3
Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor	3
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter	3
Influence of innovative hydrogen multi strut injector with different spacing on cavity-based scramjet combustor	3
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber	3
Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins	3
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor	2
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine	2
Expanding the choke margin of a mixed flow compressor stage for a micro gas turbine engine	2
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment	2
Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation	2
Research on a high-precision real-time improvement method for aero-engine component-level model	2

Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application	2
Supersonic jet mixing in the presence of two annular co-flow streams	2
Control of subsonic jets using vanes as vortex generators	2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions	2
Dynamic characteristics of open-ends squeeze film dampers with air ingestion	2
A new compilation method of general standard test load spectrum for aircraft engine	2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions	2
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients	2
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper	2
Improving thermal performance of turbine blade with combination of circular and oblong fins in a wedge channel: a numerical investigation	2
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser	2
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor	2
Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario	2
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence	2
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper	1
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties	1
Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor	1
Multi-condition design optimization of groove flow control technique in an axial-flow pump	1
Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade	1
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity	1
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC	1
Active fault tolerant control of turbofan engines with actuator faults under disturbances	1
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates	1
Simulation and analysis of an aero-engine combustor with a slinger fuel injection system	1
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis	1
Characterization of titanium grade 5 alloy compressor blade in a jet engine using advanced materials for optimum thrust production	1
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine	1
Research on a component characteristic adaptive correction method for variable cycle engines	1
Study of the vortex chamber and its application for the development of novel measurement and control devices	1
Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex	1
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions	1
Detailed investigation of supersonic film cooling performance in a convergent divergent nozzle	1
Investigation on flow characteristics and its effect on heat transfer enhancement in a wedge channel with combination of circular, oblong, teardrop, and pencil pin fins	1
Characterization of titanium grade 5 alloy compressor blade in a jet engine using advanced materials for optimum thrust production	1
Numerical analysis of high temperature gas flow through conical micronozzle	1
An improved aerodynamic performance optimization method of 3-D low Reynolds number rotor blade	1
Optimization of ACE mode transition control schedule considering geometric adjustment speed	1
Analysis on impulse characteristics of pulse detonation engine with nozzles	1
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications	1
Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature	1
The influence of the geometry of V-gutter bluff body on transient vortex shedding	1
Modeling and validation of the volume effect on the axial fan transient performance	1
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor	1
An improved compact propulsion system model based on batch normalize deep neural network	1
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine	1
Design and analysis of air intake of subsonic cruise vehicle with experimental validation	1
The role of volume effect on the transient behavior of a transonic compressor	1
Research on the influence of honeycomb cell blockage on the seal leakage characteristics	1
Modeling and analysis of 3D radiative heat transfer in combustor	1
Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils	1

Influence of nozzle exit geometrical parameters on supersonic jet decay	1
Optimization of a circumferential groove in a centrifugal compressor	1
Parametric analysis of thermal cycle of a short take-off and vertical landing engine	1
Predicting compressor mass flow rate using various machine learning approaches	1
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine	1
Experimental and numerical study of flame structure and emissions in a micro gas turbine combustor	1
Active fault tolerant control of turbofan engines with actuator faults under disturbances	1
Control-oriented quasi-one dimensional modeling method for scramjet	1
Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application	1
Impact of cavity and ramp configuration on the combustion performance of a strut-based scramjet combustor	1