International Journal of Turbo & Jet-Engines

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 2020-07-01 to 2024-07-01.)
ArticleCitations
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview11
Exergy analysis of a turboprop engine at different flight altitude and speeds using novel consideration8
Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel7
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine6
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser6
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration5
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage4
One-equation turbulence models applied to practical scramjet inlet3
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients3
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview3
A new method to improve the real-time performance of aero-engine component level model3
Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel3
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach3
Predicting remaining useful life of turbofan engines using degradation signal based echo state network3
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber3
A Study on the Effect of Angle in Diffused Hole Film Cooling Effectiveness at Different Blowing Ratios2
Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins2
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment2
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor2
Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions2
Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel2
Control of subsonic jets using vanes as vortex generators2
Experimental research on the performance of the forward variable area bypass injector for variable cycle engines2
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser2
Effect of multi-hole arrangement on the effusion cooling with backward injection2
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients2
Experimental research on the performance of the forward variable area bypass injector for variable cycle engines2
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper2
Study on Influence of Diameter on Detonation Acoustic Characteristics of Pulse Detonation Engine2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions2
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter2
Modeling and mode transition simulation of over-under turbine based combined cycle (TBCC) propulsion system based on inlet/engine matching2
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system2
Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation2
Research on a high-precision real-time improvement method for aero-engine component-level model2
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor2
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions1
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties1
A new method to improve the real-time performance of aero-engine component level model1
Modeling and analysis of 3D radiative heat transfer in combustor1
Optimization of a circumferential groove in a centrifugal compressor1
Influence of nozzle exit geometrical parameters on supersonic jet decay1
Experimental and numerical study of flame structure and emissions in a micro gas turbine combustor1
Optimization of ACE mode transition control schedule considering geometric adjustment speed1
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine1
Active fault tolerant control of turbofan engines with actuator faults under disturbances1
Simulation and analysis of an aero-engine combustor with a slinger fuel injection system1
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates1
Control-oriented quasi-one dimensional modeling method for scramjet1
An active fault-tolerant control strategy of aircraft engines based on multi-model predictive control1
Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex1
Improving thermal performance of turbine blade with combination of circular and oblong fins in a wedge channel: a numerical investigation1
Expanding the choke margin of a mixed flow compressor stage for a micro gas turbine engine1
Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils1
Numerical analysis of high temperature gas flow through conical micronozzle1
Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model1
Research on the influence of honeycomb cell blockage on the seal leakage characteristics1
A new compilation method of general standard test load spectrum for aircraft engine1
Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model1
Analysis on impulse characteristics of pulse detonation engine with nozzles1
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC1
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence1
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine1
Active fault tolerant control of turbofan engines with actuator faults under disturbances1
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications1
Supersonic jet mixing in the presence of two annular co-flow streams1
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine1
Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application1
Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor1
Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor1
An improved aerodynamic performance optimization method of 3-D low Reynolds number rotor blade1
A study on design optimization for compressor blisks1
Conjugate heat transfer analysis of a radially cooled nozzle guide vane in an aero gas turbine engine1
Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade1
Influence of innovative hydrogen multi strut injector with different spacing on cavity-based scramjet combustor1
Characterization of titanium grade 5 alloy compressor blade in a jet engine using advanced materials for optimum thrust production1
Modeling and validation of the volume effect on the axial fan transient performance1
The influence of the geometry of V-gutter bluff body on transient vortex shedding1
Research on a component characteristic adaptive correction method for variable cycle engines1
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis1
Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature1
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine1
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper1
An improved compact propulsion system model based on batch normalize deep neural network1
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