International Journal of Turbo & Jet-Engines

Papers
(The TQCC of International Journal of Turbo & Jet-Engines is 2. 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 2022-01-01 to 2026-01-01.)
ArticleCitations
Frontmatter44
Design optimization of a fluidic thrust vectoring system based on coanda effect using meta-models18
Numerical study of transition process in different zones of a compressor cascade channel16
Uncertainty propagation in transient heat transfer from an extended surface11
Investigation of flow and thermal behavior in multi-stage high-pressure compressor disk cavities10
Research on real-time improvement method of on-board physical mechanism model of turboshaft engine based on neural network10
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade9
Performance enhancement and flow separation control in an S-duct by air injection9
Role of different cavity flame holders on the performance characteristics of supersonic combustor8
Application of KH-RT model in lifting flame of methanol jet atomization7
Active subspace-based performance analysis of supersonic through-flow fan rotor7
Frontmatter6
Investigations of modified cooling hole injection angle configurations for improved trench film cooling performance6
Numerical study of effect of the casing slot on the tip leakage vortex and vortex cavitation of a fuel pump6
Detailed investigation of supersonic film cooling performance in a convergent divergent nozzle6
Frontmatter6
Study of a new effervescent atomizer design6
Innovative modification of the NACA 0012 airfoil for enhanced lift and aerodynamic efficiency: CFD and experimental validation6
C conjugate heat transfer simulation of swirl internal cooling on blade leading edge6
Performance analysis of a gas turbine engine with intercooling and regeneration process - Part 16
Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters5
Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan5
Control of subsonic jets using vanes as vortex generators5
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence4
Research on adjoint-based customized integrated passage design of Rotor 674
Aerothermal effects of squealer openings on a cavity tip in a turbine cascade4
A cooled turbine airfoil performance prediction method with two-dimensional CFD computation and loss models4
Frontmatter4
Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis4
Influence mechanism of advance ratio on the aerodynamic performance of a contra-rotating propfan4
A new schedule method for compact propulsion system model4
Research on high-bandwidth linear active disturbance rejection control method for variable speed turboshaft engine4
Influences of unbalance phase combination on the dynamic characteristics for a turboprop engine4
Computational analysis of the scramjet mode of the RBCC inlet using micro vortex generators4
Simulation and analysis of the over-expanded flow field in asymmetric nozzles with lateral expansion3
Study on laser de-weight and dynamic balance technology of rotating machines3
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage3
Influence of conical shaft stiffness on the dynamic characteristics of flexible rotor3
Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification3
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity3
Turbojet module sizing for integration with turbine-based combined cycle engine3
Influence of non-axisymmetric endwall profiling under incoming vortex on the corner separation of a diffusion cascade3
Numerical investigation of a novel mushroom-shaped cooling hole for enhanced film cooling performance3
Research on turboprop engine control method based on linear parameter varying model3
Flow field characteristics of isolator with fluidic injection3
Infrared simulation of aircraft rear fuselage based on a coupled CFD method3
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration3
Numerical investigation of ice crystal melting characteristic and icing risk in an axial compressor2
A high-dimensional and high-precision onboard modeling method for adaptive variable cycle engine2
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system2
Research on a high-precision real-time improvement method for aero-engine component-level model2
A study on optimal rotor speed control method for helicopter power system considering the influence of infrared suppressors2
Impact of annular ribs in sudden expansion flow conditions to control base pressure2
Effect of free boundary on the performance of single expansion nozzle2
Design and analysis of air intake of subsonic cruise vehicle with experimental validation2
Performance analysis of a planar shaped strut injector based supersonic combustion chamber2
Air tab location effect on supersonic jet mixing2
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions2
Integration of multi module flow domain to demonstrate the full engine aero-flow path simulation of Single Spool Turbojet Engine2
Research on cascade control method for turboshaft engine with variable rotor speed2
Frontmatter2
Modeling and validation of the volume effect on the axial fan transient performance2
Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine2
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity2
Study of vortex throttle characteristics with adjustable resistance by rotation of the vortex chamber inlet channel2
Numerical investigation on mixing of heated confined swirling coaxial jets with blockage2
Performance study of bypass dual throat nozzle based on numerical simulation2
Uncertainty quantification of leakage characteristics of stepped labyrinth seals based on sparse PC-Kriging model2
Frontmatter2
Installed performance seeking control based on supersonic variable inlet/engine coupling model2
An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil2
Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall2
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties2
A torsional vibration coupling dynamic modeling and analysis method for engine/power transmission systems in coaxial high-speed helicopters2
A novel degradation estimation of lifecycle health monitoring for aircraft engine gas path rotational components2
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