International Journal of Turbo & Jet-Engines

Papers
(The median citation count of International Journal of Turbo & Jet-Engines is 0. 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 2021-05-01 to 2025-05-01.)
ArticleCitations
Frontmatter19
Numerical study of transition process in different zones of a compressor cascade channel11
Frontmatter9
Aero-thermal optimization of the rim seal cavity to enhance rotor platform thermal protection8
The influence of the geometry of V-gutter bluff body on transient vortex shedding7
Application of KH-RT model in lifting flame of methanol jet atomization6
Design optimization of a fluidic thrust vectoring system based on coanda effect using meta-models6
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade6
Effect of rotor–stator rim cavity flow on the turbine5
Performance enhancement and flow separation control in an S-duct by air injection5
Role of different cavity flame holders on the performance characteristics of supersonic combustor5
Active subspace-based performance analysis of supersonic through-flow fan rotor5
Investigations of modified cooling hole injection angle configurations for improved trench film cooling performance4
Frontmatter4
Detailed investigation of supersonic film cooling performance in a convergent divergent nozzle4
C conjugate heat transfer simulation of swirl internal cooling on blade leading edge4
Performance analysis of a gas turbine engine with intercooling and regeneration process - Part 13
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine3
Frontmatter3
Numerical study of effect of the casing slot on the tip leakage vortex and vortex cavitation of a fuel pump3
Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan3
Control of subsonic jets using vanes as vortex generators3
Study of a new effervescent atomizer design3
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper3
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity2
Computational analysis of the scramjet mode of the RBCC inlet using micro vortex generators2
Frontmatter2
A new schedule method for compact propulsion system model2
Aerothermal effects of squealer openings on a cavity tip in a turbine cascade2
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
Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis2
Research on high-bandwidth linear active disturbance rejection control method for variable speed turboshaft engine2
Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters2
Simulation and analysis of the over-expanded flow field in asymmetric nozzles with lateral expansion2
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach2
Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification2
Study of vortex throttle characteristics with adjustable resistance by rotation of the vortex chamber inlet channel2
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor2
A cooled turbine airfoil performance prediction method with two-dimensional CFD computation and loss models2
Influences of unbalance phase combination on the dynamic characteristics for a turboprop engine2
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence2
Research on turboprop engine control method based on linear parameter varying model2
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage2
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates1
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system1
Frontmatter1
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties1
Installed performance seeking control based on supersonic variable inlet/engine coupling model1
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions1
Frontmatter1
Design and analysis of air intake of subsonic cruise vehicle with experimental validation1
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration1
Design and validation of a two-dimensional variable geometry inlet1
Performance analysis of a planar shaped strut injector based supersonic combustion chamber1
Assessment of performance degradation of a mixed flow low bypass turbofan engine through GasTurb simulation1
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC1
Review of gliding arc plasma assisted ignition and combustion for gas turbine application1
Research on cascade control method for turboshaft engine with variable rotor speed1
Impact of annular ribs in sudden expansion flow conditions to control base pressure1
An improved compact propulsion system model based on batch normalize deep neural network1
A study on optimal rotor speed control method for helicopter power system considering the influence of infrared suppressors1
Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall1
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity1
Influence of conical shaft stiffness on the dynamic characteristics of flexible rotor1
Infrared simulation of aircraft rear fuselage based on a coupled CFD method1
A novel degradation estimation of lifecycle health monitoring for aircraft engine gas path rotational components1
An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil1
A part-load performance analysis method for gas turbines based on the stage by stages model of the power turbine1
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
Dynamic characteristics of open-ends squeeze film dampers with air ingestion1
Research on a high-precision real-time improvement method for aero-engine component-level model1
Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine1
Modeling and validation of the volume effect on the axial fan transient performance1
Numerical investigation of ice crystal melting characteristic and icing risk in an axial compressor1
Modeling and analysis of 3D radiative heat transfer in combustor1
Air tab location effect on supersonic jet mixing1
Numerical investigation on mixing of heated confined swirling coaxial jets with blockage1
Effect of free boundary on the performance of single expansion nozzle1
Research on a component characteristic adaptive correction method for variable cycle engines1
Effects of bleed pressure on shock-wave/boundary-layer interactions in a transonic compressor stator with suction holes0
Probabilistic analysis of maximum mode shape for mistuned blisk0
Study on one-dimensional performance prediction of multi-stage axial turbine based on the blade height0
Research on vibration damping of integral squeeze film damper based on fan rotor tester of turbofan0
Compensator based improved model predictive control for Aero-engine0
Virtual deflection with synthetic jet actuators at high angles of attack0
Study on the water ingestion performance of compressor with inlet particle separator0
Flow structure comparison of film cooling versus hybrid cooling: a CFD study0
Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft0
Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application0
Speed controller design for turboshaft engine using a high-fidelity AeroThermal model0
Conjugate heat transfer analysis on double-wall cooling configuration including jets impingement and film holes with conformal pins0
Predicting remaining useful life of turbofan engines using degradation signal based echo state network0
Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins0
Frontmatter0
Sensitivity analysis of aero-engine performance optimization control system and its hardware test verification0
Analysis of leakage characteristics and structural optimization of two-stage floating ring seal0
Gas dynamic analysis of the modern single shaft gas turbine engine flow path0
Effect of inlet diameter on the flow structure and performance for aluminum-based water-jet engine0
A creep-fatigue life prediction model considering multi-factor coupling effect0
Simulation and analysis of hot plume infrared signature based on SNB model0
The aerothermal performance of turbine blade squealer tip at various Reynolds numbers and Mach numbers with moving endwall0
Quantitative investigation of the evaporation and resistance characteristics of inlet jet precooling0
Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application0
Numerical simulations of a turbulent lifted hydrogen flame in vitiated coflow with flamelet generated manifold approach0
Design optimization of a supersonic through-flow fan rotor based on the blade profiles0
Probabilistic analysis of solid oxide fuel-cell integrated with gas turbine0
Frontmatter0
Analysis on impulse characteristics of pulse detonation engine with nozzles0
Simple model of turbine-based combined cycle propulsion system and smooth mode transition0
Numerical and experimental study on the critical geometric variation based on sensitivity analysis on a compressor rotor0
Impact investigation of inlet environmental changes on the rated condition performance of a high-pressure compressor0
Flow pattern formation due to the interdependency of multi-component interactions and their impact on the performance of turbine and exhaust duct of gas turbine0
Effect of asymmetric leading edge on transition of suction side0
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview0
Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation0
Upgraded one-dimensional code for the design of a micro gas turbine mixed flow compressor stage with various crossover diffuser configurations0
Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor0
Multi-nozzle thrust matching control of STOVL engine0
Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade0
Supersonic jet mixing in the presence of two annular co-flow streams0
Performance analysis of a gas turbine engine via intercooling and regeneration- Part 20
Multi-condition design optimization of groove flow control technique in an axial-flow pump0
Influence of metal magnesium addition on detonation initiation in shock wave focusing Pulse Detonation Engine0
Frontmatter0
Investigation on effect of injector orifice diameter on injector atomization and combustion characteristics of pulse detonation combustor0
A novel design methodology for preventing dislocation in the Zig-zag shroud0
Aero-engine direct thrust control based on nonlinear model predictive control with composite predictive model0
Frontmatter0
Parametric analysis of thermal cycle of a short take-off and vertical landing engine0
Ignition experimental study based on rotating gliding arc0
Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor0
Research on the design method of mode transition control law for Ma6 external parallel TBCC engine0
Expanding the choke margin of a mixed flow compressor stage for a micro gas turbine engine0
The design method of the V-shaped groove piston ring0
Multi-objective optimization of the aerodynamic performance of butterfly-shaped film cooling holes in rocket thrust chamber0
The overall film cooling performance of crescent holes0
Performance analysis of pulse detonation ramjet0
Influence of inlet structure on combustion flow structure in magnesium powder fueled water ramjet engine0
Frontmatter0
Deep residual ensemble model for predicting remaining useful life of turbo fan engines0
Applicability of correlational data-mining to small-scale turbojet performance map generation0
Frontmatter0
Research on performance seeking control of turbofan engine in minimum hot spot temperature mode0
Experimental and numerical study of flame structure and emissions in a micro gas turbine combustor0
Numerical investigation of flow control in low-pressure turbine cascade using Gurney Flaps0
Numerical and experimental investigations of tip clearance effects in a high-flow-coefficient centrifugal compressor0
Numerical analysis of brush seal hysteresis based on orthogonal test method0
Frontmatter0
A novel design of impeller cavity pre-swirl system for efficient supercharging and low power consumption0
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser0
Study of the vortex chamber and its application for the development of novel measurement and control devices0
A new compilation method of general standard test load spectrum for aircraft engine0
Effect of the distribution of the upstream probe support on performance of compressor cascade0
Vortex structure control based bleed in axial compressor cascade with tip clearance using large eddy simulation0
Experimental study on flow field and combustion characteristics of V-gutter and integrated flameholders0
Influence of innovative hydrogen multi strut injector with different spacing on cavity-based scramjet combustor0
In-service load calculation surrogate models for high-pressure turbine blade life digital twin0
Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex0
Numerical analysis on the effect of passive control geometry in supersonic jet mixing enhancement0
Research on the influence of honeycomb cell blockage on the seal leakage characteristics0
Effect of bypass ratio on sonic underexpanded co-flow jets with finite lip thickness0
Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel0
Design of mode transition control system for tandem TBCC engine based on direct performance parameters closed-loop control0
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor0
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine0
Optimization and numerical investigation of combined design of blade and endwall on rotor 670
Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils0
The International Journal of Turbo and Jet Engines0
Thermal performance of teardrop pin fins and zig zag ribs in a wedge channel0
Influence of the ending position of controllable speed casing on a transonic compressor rotor tip leakage flow0
Effect of lip-thickness on rectangular nozzle co-flowing subsonic jet0
Effect of tab shape, length, and placement on the over-expanded free jet at Mach 2.00
Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor0
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment0
The aerodynamic performance degradation analysis of a small high bypass turbofan engine compression system with fan rotor blade leading edge erosion0
A study on design optimization for compressor blisks0
The role of volume effect on the transient behavior of a transonic compressor0
Research on new integral squeeze film damper vibration control of micro turbojet engine at high speed0
Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors0
Numerical investigation of tip clearance flow in a variable geometry turbine with non-uniform partial clearance0
Research on temperature rise characteristics of end V-groove ring seal0
Thrust-matching and optimization design of turbine-based combined cycle engine with trajectory optimization0
Design and combustion characteristics analysis of a static shaft turbofan engine0
Constant temperature line identification on prototype gas turbine combustor with multi-colour change coating0
Uncertainty quantification by probabilistic analysis of circular fins0
Finite element based dynamic analysis of a porous exponentially graded shaft system subjected to thermal gradients0
Effect of preheated swirling multi-annular jets on mixing and flow characteristics in various expanded confinements0
Integrated modeling and coupling characteristics analysis of helicopter/engine/infrared suppressor0
Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine0
Effects of turbulence and flamelet combustion modelling on the CFD simulation of a dual inlet ramjet combustor0
The study of cascading effect in the integration of intake with gas turbine engine bay in subsonic cruise vehicle0
Effect of velocity ratio and Mach number on thin lip coaxial jet0
An improved aerodynamic performance optimization method of 3-D low Reynolds number rotor blade0
Conjugated heat transfer characteristics of ribbed-swirl cooling in turbine blade under rotation condition0
Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field0
Flight trajectory optimization study of a variable-cycle turbine-based combined cycle engine hypersonic vehicle based on airframe/engine integration0
Frontmatter0
Numerical study of the impact of hydrogen addition, swirl intensity and equivalence ratio on methane-air combustion0
Effect of tab shape, length, and placement on the over-expanded free jet at Mach 2.00
CFD analysis of flow control in compressor cascade using MVGs0
The aerothermodynamic cycle optimal design of a turbofan engine0
Improving thermal performance of turbine blade with combination of circular and oblong fins in a wedge channel: a numerical investigation0
Frontmatter0
Effect of multi-hole arrangement on the effusion cooling with backward injection0
Numerical investigation of force over the horizontal jet tab of various sector angle fixed to the convergent-divergent nozzle exit0
Multi-parameter study on array-jets impingement with crossflow temperature effect0
Probabilistic analysis of blade flutter based on particle swarm optimization-deep extremum neural network0
Numerical study on the effect of distortion of S-duct on flow field and performance of a full annulus transonic fan0
Research on an optimization design method for a TBCC propulsion scheme0
Optimization of a circumferential groove in a centrifugal compressor0
Hypersonic boundary layer flow at an axisymmetric stagnation point on a blunt body0
Optimization of ACE mode transition control schedule considering geometric adjustment speed0
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications0
Exploration of shock-induced flow dynamics and turbulence-driven combustion optimization in advanced cavity configurations of hydrogen fueled scramjet combustors0
Hot gas ingestion in chute rim seal clearance of gas turbine0
Predicting compressor mass flow rate using various machine learning approaches0
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter0
Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature0
Investigation of effect of atomization performance on lean blowout limit for gas turbine combustors by comparison of utilizing aviation kerosene and methane as fuel0
Numerical analysis of pollutant formation and exhaust emission in a short annular combustor under part load operation0
Comparative study of numerical approaches to adaptive gas turbine cycle analysis0
Impact of cavity and ramp configuration on the combustion performance of a strut-based scramjet combustor0
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis0
One-equation turbulence models applied to practical scramjet inlet0
Experimental and numerical investigations on controlled parameter selection methods for kerosene-fueled scramjet0
Optimization of labyrinth seal leakage with independently varied tooth parameters using efficient global optimization0
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine0
Computational assessment of performance parameters of an aero gas turbine combustor for full flight envelope operation0
Effect of perforated wall in controlling the separation due to SWBLI at Mach no. 5 to 90
Integrated design and analysis of inlet and missile with two side layout0
Fluid flow in a microdiffuser at small Reynolds numbers0
Numerical study on aerodynamic performance of an intake duct affected by ground effect0
Frontmatter0
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