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 2020-12-01 to 2024-12-01.)
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 Consideration7
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview6
Predicting remaining useful life of turbofan engines using degradation signal based echo state network5
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 inlet4
Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel4
Influence of innovative hydrogen multi strut injector with different spacing on cavity-based scramjet combustor3
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients3
A study on design optimization for compressor blisks3
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter3
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach3
Improving thermal performance of turbine blade with combination of circular and oblong fins in a wedge channel: a numerical investigation3
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions3
Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins3
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system3
Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor3
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber3
Effect of multi-hole arrangement on the effusion cooling with backward injection3
Research on a high-precision real-time improvement method for aero-engine component-level model2
Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application2
Control of subsonic jets using vanes as vortex generators2
Supersonic jet mixing in the presence of two annular co-flow streams2
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment2
A new compilation method of general standard test load spectrum for aircraft engine2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions2
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper2
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients2
Expanding the choke margin of a mixed flow compressor stage for a micro gas turbine engine2
Dynamic characteristics of open-ends squeeze film dampers with air ingestion2
Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation2
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence2
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine2
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor2
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser2
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor2
Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature1
The influence of the geometry of V-gutter bluff body on transient vortex shedding1
Control-oriented quasi-one dimensional modeling method for scramjet1
Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application1
Impact of cavity and ramp configuration on the combustion performance of a strut-based scramjet combustor1
An improved compact propulsion system model based on batch normalize deep neural network1
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions1
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties1
Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade1
Influence of nozzle exit geometrical parameters on supersonic jet decay1
An improved aerodynamic performance optimization method of 3-D low Reynolds number rotor blade1
Optimization of ACE mode transition control schedule considering geometric adjustment speed1
Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils1
Predicting compressor mass flow rate using various machine learning approaches1
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine1
Experimental and numerical study of flame structure and emissions in a micro gas turbine combustor1
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine1
Research on a component characteristic adaptive correction method for variable cycle engines1
Study of the vortex chamber and its application for the development of novel measurement and control devices1
Design and analysis of air intake of subsonic cruise vehicle with experimental validation1
Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor1
Multi-condition design optimization of groove flow control technique in an axial-flow pump1
Numerical analysis of high temperature gas flow through conical micronozzle1
Parametric analysis of thermal cycle of a short take-off and vertical landing engine1
Optimization of a circumferential groove in a centrifugal compressor1
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity1
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates1
Simulation and analysis of an aero-engine combustor with a slinger fuel injection system1
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis1
Modeling and validation of the volume effect on the axial fan transient performance1
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor1
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper1
Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex1
Detailed investigation of supersonic film cooling performance in a convergent divergent nozzle1
The role of volume effect on the transient behavior of a transonic compressor1
Modeling and analysis of 3D radiative heat transfer in combustor1
Research on the influence of honeycomb cell blockage on the seal leakage characteristics1
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
Analysis on impulse characteristics of pulse detonation engine with nozzles1
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications1
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine0
Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis0
Probabilistic analysis of solid oxide fuel-cell integrated with gas turbine0
Study of a new effervescent atomizer design0
Effect of velocity ratio and Mach number on thin lip coaxial jet0
Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine0
Conjugate heat transfer analysis on double-wall cooling configuration including jets impingement and film holes with conformal pins0
Thermal performance of teardrop pin fins and zig zag ribs in a wedge channel0
Integrated design and analysis of inlet and missile with two side layout0
Effect of multi-hole arrangement on the effusion cooling with backward injection0
Speed controller design for turboshaft engine using a high-fidelity AeroThermal model0
Numerical study on the effect of distortion of S-duct on flow field and performance of a full annulus transonic fan0
Experimental and numerical investigations on controlled parameter selection methods for kerosene-fueled scramjet0
Performance analysis of a gas turbine engine via intercooling and regeneration- Part 20
Computational analysis of the scramjet mode of the RBCC inlet using micro vortex generators0
Simulation and analysis of hot plume infrared signature based on SNB model0
Ignition experimental study based on rotating gliding arc0
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
Simple model of turbine-based combined cycle propulsion system and smooth mode transition0
Hot gas ingestion in chute rim seal clearance of gas turbine0
Deep residual ensemble model for predicting remaining useful life of turbo fan engines0
A novel design of impeller cavity pre-swirl system for efficient supercharging and low power consumption0
Numerical investigation of ice crystal melting characteristic and icing risk in an axial compressor0
Experimental investigation on mixing characteristics of high speed co-flow jets by using tabbed chevron nozzle0
Vortex structure control based bleed in axial compressor cascade with tip clearance using large eddy simulation0
Numerical and experimental study on the critical geometric variation based on sensitivity analysis on a compressor rotor0
Frontmatter0
Applicability of correlational data-mining to small-scale turbojet performance map generation0
Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters0
Infrared simulation of aircraft rear fuselage based on a coupled CFD method0
Numerical study of the impact of hydrogen addition, swirl intensity and equivalence ratio on methane-air combustion0
Numerical investigation of flow control in low-pressure turbine cascade using Gurney Flaps0
A study on optimal rotor speed control method for helicopter power system considering the influence of infrared suppressors0
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine0
The aerodynamic performance degradation analysis of a small high bypass turbofan engine compression system with fan rotor blade leading edge erosion0
Compensator based improved model predictive control for Aero-engine0
Optimization of ACE mode transition control schedule considering geometric adjustment speed0
Design optimization of a supersonic through-flow fan rotor based on the blade profiles0
Impact investigation of inlet environmental changes on the rated condition performance of a high-pressure compressor0
Effect of tab shape, length, and placement on the over-expanded free jet at Mach 2.00
Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor0
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity0
Research on an optimization design method for a TBCC propulsion scheme0
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber0
Fluid flow in a microdiffuser at small Reynolds numbers0
The International Journal of Turbo and Jet Engines0
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence0
Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall0
Application of KH-RT model in lifting flame of methanol jet atomization0
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties0
Research on turboprop engine control method based on linear parameter varying model0
Frontmatter0
Influence of nozzle exit geometrical parameters on supersonic jet decay0
Numerical and experimental investigations of tip clearance effects in a high-flow-coefficient centrifugal compressor0
Frontmatter0
Flight trajectory optimization study of a variable-cycle turbine-based combined cycle engine hypersonic vehicle based on airframe/engine integration0
C conjugate heat transfer simulation of swirl internal cooling on blade leading edge0
Virtual deflection with synthetic jet actuators at high angles of attack0
Study on laser de-weight and dynamic balance technology of rotating machines0
Influences of unbalance phase combination on the dynamic characteristics for a turboprop engine0
Sensitivity analysis of aero-engine performance optimization control system and its hardware test verification0
Frontmatter0
Effect of tab shape, length, and placement on the over-expanded free jet at Mach 2.00
Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft0
A new schedule method for compact propulsion system model0
Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan0
Air tab location effect on supersonic jet mixing0
Design and validation of a two-dimensional variable geometry inlet0
Frontmatter0
Research on a component characteristic adaptive correction method for variable cycle engines0
Influence of metal magnesium addition on detonation initiation in shock wave focusing Pulse Detonation Engine0
Investigation on effect of injector orifice diameter on injector atomization and combustion characteristics of pulse detonation combustor0
Frontmatter0
Frontmatter0
Research on the design method of mode transition control law for Ma6 external parallel TBCC engine0
Constant temperature line identification on prototype gas turbine combustor with multi-colour change coating0
CFD analysis of flow control in compressor cascade using MVGs0
Research on quasi-one-dimensional modeling and performance analysis of RBCC propulsion system0
Experimental study on flow field and combustion characteristics of V-gutter and integrated flameholders0
Study of a new effervescent atomizer design0
Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification0
Numerical investigation of flow control in low-pressure turbine cascade using Gurney Flaps0
Quantitative investigation of the evaporation and resistance characteristics of inlet jet precooling0
Performance enhancement and flow separation control in an S-duct by air injection0
Multi-objective optimization of the aerodynamic performance of butterfly-shaped film cooling holes in rocket thrust chamber0
Installed performance seeking control based on supersonic variable inlet/engine coupling model0
Frontmatter0
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions0
Numerical investigation of force over the horizontal jet tab of various sector angle fixed to the convergent-divergent nozzle exit0
Research on quasi-one-dimensional modeling and performance analysis of RBCC propulsion system0
Investigation of effect of atomization performance on lean blowout limit for gas turbine combustors by comparison of utilizing aviation kerosene and methane as fuel0
Hot gas ingestion in chute rim seal clearance of gas turbine0
Effects of turbulence and flamelet combustion modelling on the CFD simulation of a dual inlet ramjet combustor0
Aero-thermal optimization of the rim seal cavity to enhance rotor platform thermal protection0
Numerical investigation of tip clearance flow in a variable geometry turbine with non-uniform partial clearance0
Numerical study on aerodynamic performance of an intake duct affected by ground effect0
Active subspace-based performance analysis of supersonic through-flow fan rotor0
Influence of the ending position of controllable speed casing on a transonic compressor rotor tip leakage flow0
Effect of bypass ratio on sonic underexpanded co-flow jets with finite lip thickness0
Analysis on impulse characteristics of pulse detonation engine with nozzles0
Performance characteristics of flow in annular diffuser using CFD0
Frontmatter0
Effect of inlet diameter on the flow structure and performance for aluminum-based water-jet engine0
Performance analysis of a planar shaped strut injector based supersonic combustion chamber0
One-equation turbulence models applied to practical scramjet inlet0
Comparative study of numerical approaches to adaptive gas turbine cycle analysis0
Effect of the distribution of the upstream probe support on performance of compressor cascade0
Frontmatter0
Study of vortex throttle characteristics with adjustable resistance by rotation of the vortex chamber inlet channel0
An improved aerodynamic performance optimization method of 3-D low Reynolds number rotor blade0
Performance analysis of pulse detonation ramjet0
Frontmatter0
Integrated modeling and coupling characteristics analysis of helicopter/engine/infrared suppressor0
Numerical study of transition process in different zones of a compressor cascade channel0
Study on the water ingestion performance of compressor with inlet particle separator0
Numerical analysis of brush seal hysteresis based on orthogonal test method0
Probabilistic analysis of maximum mode shape for mistuned blisk0
Design and combustion characteristics analysis of a static shaft turbofan engine0
Research on new integral squeeze film damper vibration control of micro turbojet engine at high speed0
Optimization and numerical investigation of combined design of blade and endwall on rotor 670
Upgraded one-dimensional code for the design of a micro gas turbine mixed flow compressor stage with various crossover diffuser configurations0
Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine0
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade0
Multi-nozzle thrust matching control of STOVL engine0
Effect of rotor–stator rim cavity flow on the turbine0
Effects of bleed pressure on shock-wave/boundary-layer interactions in a transonic compressor stator with suction holes0
Computational assessment of performance parameters of an aero gas turbine combustor for full flight envelope operation0
Research on performance seeking control of turbofan engine in minimum hot spot temperature mode0
Comparative study of numerical approaches to adaptive gas turbine cycle analysis0
Finite element based dynamic analysis of a porous exponentially graded shaft system subjected to thermal gradients0
Conjugated heat transfer characteristics of ribbed-swirl cooling in turbine blade under rotation condition0
A cooled turbine airfoil performance prediction method with two-dimensional CFD computation and loss models0
Performance analysis of a gas turbine engine with intercooling and regeneration process - Part 10
Role of different cavity flame holders on the performance characteristics of supersonic combustor0
Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field0
Simulation and analysis of an aero-engine combustor with a slinger fuel injection system0
Probabilistic analysis of blade flutter based on particle swarm optimization-deep extremum neural network0
Research on temperature rise characteristics of end V-groove ring seal0
Aero-engine direct thrust control based on nonlinear model predictive control with composite predictive model0
The aerothermal performance of turbine blade squealer tip at various Reynolds numbers and Mach numbers with moving endwall0
A creep-fatigue life prediction model considering multi-factor coupling effect0
Effect of the distribution of the upstream probe support on performance of compressor cascade0
The design method of the V-shaped groove piston ring0
Assessment of performance degradation of a mixed flow low bypass turbofan engine through GasTurb simulation0
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC0
An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil0
Frontmatter0
An improved compact propulsion system model based on batch normalize deep neural network0
Numerical analysis on the effect of passive control geometry in supersonic jet mixing enhancement0
Effect of rotor–stator rim cavity flow on the turbine0
The influence of the geometry of V-gutter bluff body on transient vortex shedding0
Gas dynamic analysis of the modern single shaft gas turbine engine flow path0
Research on high-bandwidth linear active disturbance rejection control method for variable speed turboshaft engine0
Performance characteristics of flow in annular diffuser using CFD0
Uncertainty quantification by probabilistic analysis of circular fins0
Numerical investigation on mixing of heated confined swirling coaxial jets with blockage0
Flow structure comparison of film cooling versus hybrid cooling: a CFD study0
Design of mode transition control system for tandem TBCC engine based on direct performance parameters closed-loop control0
Frontmatter0
Simulation and analysis of hot plume infrared signature based on SNB model0
Gas dynamic analysis of the modern single shaft gas turbine engine flow path0
Effect of free boundary on the performance of single expansion nozzle0
Effect of perforated wall in controlling the separation due to SWBLI at Mach no. 5 to 90
Experimental investigation on mixing characteristics of high speed co-flow jets by using tabbed chevron nozzle0
Review of gliding arc plasma assisted ignition and combustion for gas turbine application0
Frontmatter0
Effect of orifice spacing on twin circular parallel compressible jets0
Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors0
Study on one-dimensional performance prediction of multi-stage axial turbine based on the blade height0
Frontmatter0
The study of cascading effect in the integration of intake with gas turbine engine bay in subsonic cruise vehicle0
Frontmatter0
Influence of inlet structure on combustion flow structure in magnesium powder fueled water ramjet engine0
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