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 2021-06-01 to 2025-06-01.)
ArticleCitations
Frontmatter21
Frontmatter11
Aero-thermal optimization of the rim seal cavity to enhance rotor platform thermal protection9
Numerical study of transition process in different zones of a compressor cascade channel7
The influence of the geometry of V-gutter bluff body on transient vortex shedding7
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade6
Design optimization of a fluidic thrust vectoring system based on coanda effect using meta-models6
Performance enhancement and flow separation control in an S-duct by air injection6
Active subspace-based performance analysis of supersonic through-flow fan rotor6
Application of KH-RT model in lifting flame of methanol jet atomization5
Frontmatter5
Role of different cavity flame holders on the performance characteristics of supersonic combustor5
C conjugate heat transfer simulation of swirl internal cooling on blade leading edge5
Performance analysis of a gas turbine engine with intercooling and regeneration process - Part 14
Study of a new effervescent atomizer design4
Frontmatter4
Detailed investigation of supersonic film cooling performance in a convergent divergent nozzle4
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper4
Investigations of modified cooling hole injection angle configurations for improved trench film cooling performance4
Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters3
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine3
Research on high-bandwidth linear active disturbance rejection control method for variable speed turboshaft engine3
Numerical study of effect of the casing slot on the tip leakage vortex and vortex cavitation of a fuel pump3
A cooled turbine airfoil performance prediction method with two-dimensional CFD computation and loss models3
Frontmatter3
Control of subsonic jets using vanes as vortex generators3
Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan3
A new schedule method for compact propulsion system model3
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach2
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence2
Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis2
Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification2
Modeling and analysis of 3D radiative heat transfer in combustor2
A novel degradation estimation of lifecycle health monitoring for aircraft engine gas path rotational components2
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage2
Simulation and analysis of the over-expanded flow field in asymmetric nozzles with lateral expansion2
Influences of unbalance phase combination on the dynamic characteristics for a turboprop engine2
Computational analysis of the scramjet mode of the RBCC inlet using micro vortex generators2
Study on laser de-weight and dynamic balance technology of rotating machines2
Influence of non-axisymmetric endwall profiling under incoming vortex on the corner separation of a diffusion cascade2
Infrared simulation of aircraft rear fuselage based on a coupled CFD method2
Influence of conical shaft stiffness on the dynamic characteristics of flexible rotor2
Research on turboprop engine control method based on linear parameter varying model2
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor2
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity2
Aerothermal effects of squealer openings on a cavity tip in a turbine cascade2
Study of vortex throttle characteristics with adjustable resistance by rotation of the vortex chamber inlet channel2
Design and validation of a two-dimensional variable geometry inlet2
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration2
Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft1
Applicability of correlational data-mining to small-scale turbojet performance map generation1
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system1
Installed performance seeking control based on supersonic variable inlet/engine coupling model1
Review of gliding arc plasma assisted ignition and combustion for gas turbine application1
An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil1
Research on a high-precision real-time improvement method for aero-engine component-level model1
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions1
Design and analysis of air intake of subsonic cruise vehicle with experimental validation1
Impact of annular ribs in sudden expansion flow conditions to control base pressure1
Assessment of performance degradation of a mixed flow low bypass turbofan engine through GasTurb simulation1
A part-load performance analysis method for gas turbines based on the stage by stages model of the power turbine1
Multi-objective optimization of the aerodynamic performance of butterfly-shaped film cooling holes in rocket thrust chamber1
Frontmatter1
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC1
Investigation on flow characteristics and its effect on heat transfer enhancement in a wedge channel with combination of circular, oblong, teardrop, and pencil pin fins1
A study on optimal rotor speed control method for helicopter power system considering the influence of infrared suppressors1
Research on a component characteristic adaptive correction method for variable cycle engines1
Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine1
Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall1
Performance analysis of a planar shaped strut injector based supersonic combustion chamber1
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties1
Research on cascade control method for turboshaft engine with variable rotor speed1
Aero-engine direct thrust control based on nonlinear model predictive control with composite predictive model1
Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field1
Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor1
Dynamic characteristics of open-ends squeeze film dampers with air ingestion1
Effect of free boundary on the performance of single expansion nozzle1
Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine1
Modeling and validation of the volume effect on the axial fan transient performance1
Numerical investigation on mixing of heated confined swirling coaxial jets with blockage1
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity1
Numerical investigation of ice crystal melting characteristic and icing risk in an axial compressor1
Air tab location effect on supersonic jet mixing1
Frontmatter1
Frontmatter1
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates1
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