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 2020-03-01 to 2024-03-01.)
ArticleCitations
The Effect of TiO2 on Engine Emissions for Gas Turbine engine Fueled with jatropha, butanol, Soya and Rapeseed Oil27
Exergetic, Exergoeconomic, Sustainability and Environmental Damage Cost Analyses of J85 Turbojet Engine with Afterburner26
Fatigue Life Prediction of Fan Blade Using Nominal Stress Method and Cumulative Fatigue Damage Theory18
Effect of Primary Rocket Jet on Thermodynamic Cycle of RBCC in Ejector Mode11
Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview10
Exergy analysis of a turboprop engine at different flight altitude and speeds using novel consideration8
Design and Numerical Investigations on a Dual-Duct Variable Geometry RBCC Inlet6
Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel6
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser6
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine6
Numerical Prediction of 45° Angled Ribs Effects on U-shaped Channels Heat Transfer and Flow under Multi Conditions5
Study on Acoustic Detection of the Working State of Pulse Detonation Engine5
The Relationship of Spike Stall and Hub Corner Separation in Axial Compressor4
Investigation of Flow Distortion Generated Forced Response of a Radial Turbine with Vaneless Volute4
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration3
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor3
One-equation turbulence models applied to practical scramjet inlet3
Dynamic Characteristics Analysis and Optimization Design of a Simulated Power Turbine Rotor Based on Finite Element Method3
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage3
Film Cooling Experimental Study on Sinusoidal Corrugated Liner for Afterburner3
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber3
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach3
Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario2
Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel2
Predicting remaining useful life of turbofan engines using degradation signal based echo state network2
Study on Influence of Diameter on Detonation Acoustic Characteristics of Pulse Detonation Engine2
Modal Analysis of the Axial Compressor Blade: Advanced Time-Dependent Electronic Interferometry and Finite Element Method2
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter2
A Research on Aero-engine Control Based on Deep Q Learning2
Aeroengine Performance Prediction Based on Double-Extremum Learning Particle Swarm Optimization2
A new method to improve the real-time performance of aero-engine component level model2
Control of subsonic jets using vanes as vortex generators2
Large-Eddy Simulation of Shaped Hole Film Cooling with the Influence of Cross Flow2
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions2
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
Evaluation of exit pattern factors of an annular aero gas turbine combustor at altitude off-design conditions2
Experimental research on the performance of the forward variable area bypass injector for variable cycle engines2
Natural frequency analysis of a functionally graded rotor-bearing system with a slant crack subjected to thermal gradients2
A Study on the Effect of Angle in Diffused Hole Film Cooling Effectiveness at Different Blowing Ratios2
Modeling and mode transition simulation of over-under turbine based combined cycle (TBCC) propulsion system based on inlet/engine matching2
Optimization of a circumferential groove in a centrifugal compressor1
Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model1
Conjugate heat transfer analysis of a radially cooled nozzle guide vane in an aero gas turbine engine1
Active fault tolerant control of turbofan engines with actuator faults under disturbances1
Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature1
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis1
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates1
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine1
Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine1
Research on Nozzle Jet Vector Control with Synthetic Jet Technology1
Experimental research on suppressing unbalanced vibration of rotor by integral squeeze film damper1
Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel1
Modeling and analysis of 3D radiative heat transfer in combustor1
Numerical analysis of high temperature gas flow through conical micronozzle1
A new compilation method of general standard test load spectrum for aircraft engine1
Experimental research on the performance of the forward variable area bypass injector for variable cycle engines1
Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model1
Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber1
Large Eddy Simulation of Secondary Flows in an Ultra-High Lift Low Pressure Turbine Cascade at Various Inlet Incidences1
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment1
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine1
Modeling and validation of the volume effect on the axial fan transient performance1
Blade Number Selection for a Splittered Mixed-Flow Compressor Impeller Using Improved Loss Model1
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
An active fault-tolerant control strategy of aircraft engines based on multi-model predictive control1
Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor1
Research on the influence of honeycomb cell blockage on the seal leakage characteristics1
Optimization of ACE mode transition control schedule considering geometric adjustment speed1
Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation1
Influence of nozzle exit geometrical parameters on supersonic jet decay1
A new method to improve the real-time performance of aero-engine component level model1
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications1
Research on a high-precision real-time improvement method for aero-engine component-level model1
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine1
The influence of the geometry of V-gutter bluff body on transient vortex shedding1
Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application1
Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex1
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor1
Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application1
Combined Flow Control of Positively Bowed Blade and Vortex Generator Jet on a Compressor Cascade1
Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor1
Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade1
Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system1
Characterization of titanium grade 5 alloy compressor blade in a jet engine using advanced materials for optimum thrust production1
An improved compact propulsion system model based on batch normalize deep neural network0
Effect of velocity ratio and Mach number on thin lip coaxial jet0
Applicability of correlational data-mining to small-scale turbojet performance map generation0
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity0
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence0
Research on quasi-one-dimensional modeling and performance analysis of RBCC propulsion system0
Research on new integral squeeze film damper vibration control of micro turbojet engine at high speed0
Conjugate heat transfer analysis on double-wall cooling configuration including jets impingement and film holes with conformal pins0
Analysis on impulse characteristics of pulse detonation engine with nozzles0
Frontmatter0
Numerical Investigation on the Cold Flow Field of a Typical Cavity-based Scramjet Combustor with Double Ramp Entry0
Optimization of ACE mode transition control schedule considering geometric adjustment speed0
A novel design of impeller cavity pre-swirl system for efficient supercharging and low power consumption0
Numerical investigation of force over the horizontal jet tab of various sector angle fixed to the convergent-divergent nozzle exit0
Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors0
Virtual deflection with synthetic jet actuators at high angles of attack0
Design of mode transition control system for tandem TBCC engine based on direct performance parameters closed-loop control0
Frontmatter0
Comparative study of numerical approaches to adaptive gas turbine cycle analysis0
Uncertainty quantification by probabilistic analysis of circular fins0
Performance characteristics of flow in annular diffuser using CFD0
Numerical investigation of flow control in low-pressure turbine cascade using Gurney Flaps0
Study of the vortex chamber and its application for the development of novel measurement and control devices0
Research on quasi-one-dimensional modeling and performance analysis of RBCC propulsion system0
Frontmatter0
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC0
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence0
Frontmatter0
Effect of orifice spacing on twin circular parallel compressible jets0
Frontmatter0
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser0
A study on optimal rotor speed control method for helicopter power system considering the influence of infrared suppressors0
Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario0
Influence of inlet structure on combustion flow structure in magnesium powder fueled water ramjet engine0
Hot gas ingestion in chute rim seal clearance of gas turbine0
One-equation turbulence models applied to practical scramjet inlet0
Characterization of titanium grade 5 alloy compressor blade in a jet engine using advanced materials for optimum thrust production0
Film cooling characteristics on a grooved surface with different injection orientation angles0
Effects of casing angle on the performance of parallel hub axial annular diffuser0
Computational assessment of performance parameters of an aero gas turbine combustor for full flight envelope operation0
Effects of casing angle on the performance of parallel hub axial annular diffuser0
Detailed investigation of supersonic film cooling performance in a convergent divergent nozzle0
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade0
Fluid flow in a microdiffuser at small Reynolds numbers0
Experimental and numerical investigation of expansion corner effects on isolator performance0
Investigation of effect of atomization performance on lean blowout limit for gas turbine combustors by comparison of utilizing aviation kerosene and methane as fuel0
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions0
Research on temperature rise characteristics of end V-groove ring seal0
Numerical study of the impact of hydrogen addition, swirl intensity and equivalence ratio on methane-air combustion0
Influences of unbalance phase combination on the dynamic characteristics for a turboprop engine0
Active fault tolerant control of turbofan engines with actuator faults under disturbances0
Probabilistic analysis of maximum mode shape for mistuned blisk0
The design method of the V-shaped groove piston ring0
Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft0
Frontmatter0
Numerical investigation of total temperature distortion problem in a multistage fan based on body force approach0
Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall0
Design and combustion characteristics analysis of a static shaft turbofan engine0
Numerical study of transition process in different zones of a compressor cascade channel0
Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis0
Simulation and analysis of hot plume infrared signature based on SNB model0
Study of a new effervescent atomizer design0
Effect of rotor–stator rim cavity flow on the turbine0
CFD analysis of flow control in compressor cascade using MVGs0
A cooled turbine airfoil performance prediction method with two-dimensional CFD computation and loss models0
Research on a component characteristic adaptive correction method for variable cycle engines0
Frontmatter0
Thermal Optimization Design of Heat Exchanger in Supersonic Engine with Parameters’ Fluctuation0
Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins0
A new schedule method for compact propulsion system model0
Quantitative investigation of the evaporation and resistance characteristics of inlet jet precooling0
Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine0
A Comparison of the Wake Effects Generated by the Biased Triangle Bar and Traditional Cylinder Bar to the Boundary Layer on Suction Surface of LPT Blade0
Control-oriented quasi-one dimensional modeling method for scramjet0
Numerical analysis on the effect of passive control geometry in supersonic jet mixing enhancement0
An active fault-tolerant control strategy of aircraft engines based on multi-model predictive control0
Effect of tab shape, length, and placement on the over-expanded free jet at Mach 2.00
Assessment of performance degradation of a mixed flow low bypass turbofan engine through GasTurb simulation0
Analysis on impulse characteristics of pulse detonation engine with nozzles0
Simulation and analysis of hot plume infrared signature based on SNB model0
Simulation and analysis of an aero-engine combustor with a slinger fuel injection system0
Experimental and numerical investigations on controlled parameter selection methods for kerosene-fueled scramjet0
Aero-thermal optimization of the rim seal cavity to enhance rotor platform thermal protection0
Effect of tab shape, length, and placement on the over-expanded free jet at Mach 2.00
Numerical study on the effect of distortion of S-duct on flow field and performance of a full annulus transonic fan0
C conjugate heat transfer simulation of swirl internal cooling on blade leading edge0
Finite element based dynamic analysis of a porous exponentially graded shaft system subjected to thermal gradients0
Frontmatter0
Frontmatter0
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment0
Integrated modeling and coupling characteristics analysis of helicopter/engine/infrared suppressor0
Effect of multi-hole arrangement on the effusion cooling with backward injection0
Experimental investigation on mixing characteristics of high speed co-flow jets by using tabbed chevron nozzle0
Frontmatter0
Impact of cavity and ramp configuration on the combustion performance of a strut-based scramjet combustor0
The aerodynamic performance degradation analysis of a small high bypass turbofan engine compression system with fan rotor blade leading edge erosion0
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Expanding the choke margin of a mixed flow compressor stage for a micro gas turbine engine0
Multi-condition design optimization of groove flow control technique in an axial-flow pump0
Influence of the ending position of controllable speed casing on a transonic compressor rotor tip leakage flow0
Aerothermal effects of squealer openings on a cavity tip in a turbine cascade0
The influence of the geometry of V-gutter bluff body on transient vortex shedding0
Numerical investigation on mixing of heated confined swirling coaxial jets with blockage0
Vortex structure control based bleed in axial compressor cascade with tip clearance using large eddy simulation0
Numerical and experimental investigations of tip clearance effects in a high-flow-coefficient centrifugal compressor0
Numerical investigation of flow control in low-pressure turbine cascade using Gurney Flaps0
Simulation and analysis of an aero-engine combustor with a slinger fuel injection system0
Numerical investigation of tip clearance flow in a variable geometry turbine with non-uniform partial clearance0
Infrared simulation of aircraft rear fuselage based on a coupled CFD method0
A creep-fatigue life prediction model considering multi-factor coupling effect0
Study of Correctly Expanded Sonic Jet with Air Tabs0
Effect of the distribution of the upstream probe support on performance of compressor cascade0
Effect of free boundary on the performance of single expansion nozzle0
Study on one-dimensional performance prediction of multi-stage axial turbine based on the blade height0
Study on laser de-weight and dynamic balance technology of rotating machines0
Optimization and numerical investigation of combined design of blade and endwall on rotor 670
Film cooling characteristics on a grooved surface with different injection orientation angles0
Numerical investigation of total temperature distortion problem in a multistage fan based on body force approach0
Flow structure comparison of film cooling versus hybrid cooling: a CFD study0
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine0
Experimental and numerical study of flame structure and emissions in a micro gas turbine combustor0
Supersonic jet mixing in the presence of two annular co-flow streams0
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties0
Frontmatter0
Dynamic characteristics of open-ends squeeze film dampers with air ingestion0
Numerical simulation of shock wave/tip leakage vortex interaction for a transonic axial fan rotor0
Effect of the distribution of the upstream probe support on performance of compressor cascade0
Integrated design and analysis of inlet and missile with two side layout0
Frontmatter0
Effects of turbulence and flamelet combustion modelling on the CFD simulation of a dual inlet ramjet combustor0
Research on a component characteristic adaptive correction method for variable cycle engines0
Frontmatter0
Study of a new effervescent atomizer design0
Design optimization of a supersonic through-flow fan rotor based on the blade profiles0
The aerothermal performance of turbine blade squealer tip at various Reynolds numbers and Mach numbers with moving endwall0
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine0
Conjugate heat transfer analysis of a radially cooled nozzle guide vane in an aero gas turbine engine0
Active subspace-based performance analysis of supersonic through-flow fan rotor0
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties0
Research on high-bandwidth linear active disturbance rejection control method for variable speed turboshaft engine0
Experimental investigation on mixing characteristics of high speed co-flow jets by using tabbed chevron nozzle0
Influence of nozzle exit geometrical parameters on supersonic jet decay0
Research on the design method of mode transition control law for Ma6 external parallel TBCC engine0
Gas dynamic analysis of the modern single shaft gas turbine engine flow path0
An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil0
Effect of rotor–stator rim cavity flow on the turbine0
The role of volume effect on the transient behavior of a transonic compressor0
Design and validation of a two-dimensional variable geometry inlet0
Frontmatter0
Numerical investigation of ice crystal melting characteristic and icing risk in an axial compressor0
Influence of metal magnesium addition on detonation initiation in shock wave focusing Pulse Detonation Engine0
Parametric analysis of thermal cycle of a short take-off and vertical landing engine0
An improved aerodynamic performance optimization method of 3-D low Reynolds number rotor blade0
Numerical study on aerodynamic performance of an intake duct affected by ground effect0
A study on design optimization for compressor blisks0
Performance characteristics of flow in annular diffuser using CFD0
Experimental and numerical investigation of expansion corner effects on isolator performance0
Frontmatter0
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions0
Performance enhancement and flow separation control in an S-duct by air injection0
Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine0
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC0
Installed performance seeking control based on supersonic variable inlet/engine coupling model0
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