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 2021-04-01 to 2025-04-01.)
ArticleCitations
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser16
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment9
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC9
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine7
The influence of the geometry of V-gutter bluff body on transient vortex shedding6
Optimization of ACE mode transition control schedule considering geometric adjustment speed6
Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification5
Multi-objective optimization of the aerodynamic performance of butterfly-shaped film cooling holes in rocket thrust chamber4
Numerical and experimental study on the critical geometric variation based on sensitivity analysis on a compressor rotor4
Aero-engine direct thrust control based on nonlinear model predictive control with composite predictive model3
A creep-fatigue life prediction model considering multi-factor coupling effect3
Research on new integral squeeze film damper vibration control of micro turbojet engine at high speed3
Frontmatter3
Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor3
CFD analysis of flow control in compressor cascade using MVGs3
Study on laser de-weight and dynamic balance technology of rotating machines3
Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine3
Applicability of correlational data-mining to small-scale turbojet performance map generation3
Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft3
Numerical study of transition process in different zones of a compressor cascade channel3
Frontmatter2
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor2
Investigation of effect of atomization performance on lean blowout limit for gas turbine combustors by comparison of utilizing aviation kerosene and methane as fuel2
Assessment of performance degradation of a mixed flow low bypass turbofan engine through GasTurb simulation2
Dynamic characteristics of open-ends squeeze film dampers with air ingestion2
Numerical and experimental investigations of tip clearance effects in a high-flow-coefficient centrifugal compressor2
Aero-thermal optimization of the rim seal cavity to enhance rotor platform thermal protection2
Numerical study of the impact of hydrogen addition, swirl intensity and equivalence ratio on methane-air combustion2
Frontmatter2
Fluid flow in a microdiffuser at small Reynolds numbers2
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates2
Design optimization of a supersonic through-flow fan rotor based on the blade profiles2
Influence of the ending position of controllable speed casing on a transonic compressor rotor tip leakage flow2
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine2
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis2
Design of mode transition control system for tandem TBCC engine based on direct performance parameters closed-loop control2
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications2
Study of vortex throttle characteristics with adjustable resistance by rotation of the vortex chamber inlet channel1
Application of KH-RT model in lifting flame of methanol jet atomization1
Conjugated heat transfer characteristics of ribbed-swirl cooling in turbine blade under rotation condition1
Performance analysis of a gas turbine engine via intercooling and regeneration- Part 21
Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field1
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter1
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage1
Role of different cavity flame holders on the performance characteristics of supersonic combustor1
Active subspace-based performance analysis of supersonic through-flow fan rotor1
The design method of the V-shaped groove piston ring1
Effect of perforated wall in controlling the separation due to SWBLI at Mach no. 5 to 91
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration1
Computational assessment of performance parameters of an aero gas turbine combustor for full flight envelope operation1
Flow pattern formation due to the interdependency of multi-component interactions and their impact on the performance of turbine and exhaust duct of gas turbine1
Investigation on effect of injector orifice diameter on injector atomization and combustion characteristics of pulse detonation combustor1
Exploration of shock-induced flow dynamics and turbulence-driven combustion optimization in advanced cavity configurations of hydrogen fueled scramjet combustors1
Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins1
Design optimization of a fluidic thrust vectoring system based on coanda effect using meta-models1
A study on design optimization for compressor blisks1
Research on temperature rise characteristics of end V-groove ring seal1
Infrared simulation of aircraft rear fuselage based on a coupled CFD method1
Performance analysis of a planar shaped strut injector based supersonic combustion chamber1
Effect of rotor–stator rim cavity flow on the turbine1
A part-load performance analysis method for gas turbines based on the stage by stages model of the power turbine1
Constant temperature line identification on prototype gas turbine combustor with multi-colour change coating1
Parametric analysis of thermal cycle of a short take-off and vertical landing engine1
Deep residual ensemble model for predicting remaining useful life of turbo fan engines1
Research on vibration damping of integral squeeze film damper based on fan rotor tester of turbofan1
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade1
Ignition experimental study based on rotating gliding arc1
Vortex structure control based bleed in axial compressor cascade with tip clearance using large eddy simulation1
Modeling and analysis of 3D radiative heat transfer in combustor1
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