OOIR: Observatory of International Research

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 2021-02-01 to 2025-02-01.)

Article	Citations
Gas dynamic analysis of the modern single shaft gas turbine engine flow path	11
The influence of the geometry of V-gutter bluff body on transient vortex shedding	7
Performance characteristics of flow in annular diffuser using CFD	6
Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor	5
Aero-thermal optimization of the rim seal cavity to enhance rotor platform thermal protection	4
Performance characteristics of flow in annular diffuser using CFD	4
Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine	4
Frontmatter	3
A creep-fatigue life prediction model considering multi-factor coupling effect	3
Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine	3
Numerical study of transition process in different zones of a compressor cascade channel	3
Frontmatter	3
CFD analysis of flow control in compressor cascade using MVGs	3
Study on laser de-weight and dynamic balance technology of rotating machines	3
Research on new integral squeeze film damper vibration control of micro turbojet engine at high speed	3
Applicability of correlational data-mining to small-scale turbojet performance map generation	3
Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft	3
Development and application of a profile loss model considering the low-Re effect in low-pressure turbine	3
Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis	2
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties	2
One-equation turbulence models applied to practical scramjet inlet	2
Influence of the ending position of controllable speed casing on a transonic compressor rotor tip leakage flow	2
Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment	2
Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor	2
Unsteady film cooling characteristics of the high-pressure turbine shroud with blade rotation in an aero-engine	2

Experimental investigation on mixing characteristics of high speed co-flow jets by using tabbed chevron nozzle	2
Fluid flow in a microdiffuser at small Reynolds numbers	2
Dynamic characteristics of open-ends squeeze film dampers with air ingestion	2
Design optimization of a supersonic through-flow fan rotor based on the blade profiles	2
Frontmatter	2
An improved aerodynamic performance optimization method of 3-D low Reynolds number rotor blade	2
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage	2
Design of mode transition control system for tandem TBCC engine based on direct performance parameters closed-loop control	2
Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates	2
Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications	2
Numerical and experimental investigations of tip clearance effects in a high-flow-coefficient centrifugal compressor	2
Multi-objective optimization of the aerodynamic performance of butterfly-shaped film cooling holes in rocket thrust chamber	1
Assessment of performance degradation of a mixed flow low bypass turbofan engine through GasTurb simulation	1
Research on vibration damping of integral squeeze film damper based on fan rotor tester of turbofan	1
Investigation on effect of injector orifice diameter on injector atomization and combustion characteristics of pulse detonation combustor	1
Modeling and analysis of 3D radiative heat transfer in combustor	1
The design method of the V-shaped groove piston ring	1
Optimization of ACE mode transition control schedule considering geometric adjustment speed	1
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade	1
Conjugated heat transfer characteristics of ribbed-swirl cooling in turbine blade under rotation condition	1
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet for TBCC	1
Design and validation of a two-dimensional variable geometry inlet	1
Design optimization of a fluidic thrust vectoring system based on coanda effect using meta-models	1
Aero-engine direct thrust control based on nonlinear model predictive control with composite predictive model	1
Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins	1
Numerical study of the impact of hydrogen addition, swirl intensity and equivalence ratio on methane-air combustion	1
The influence of the geometry of V-gutter bluff body on transient vortex shedding	1
Flow pattern formation due to the interdependency of multi-component interactions and their impact on the performance of turbine and exhaust duct of gas turbine	1
Research on temperature rise characteristics of end V-groove ring seal	1
Infrared simulation of aircraft rear fuselage based on a coupled CFD method	1
Role of different cavity flame holders on the performance characteristics of supersonic combustor	1
A study on design optimization for compressor blisks	1
Computational assessment of performance parameters of an aero gas turbine combustor for full flight envelope operation	1
Optimization of ACE mode transition control schedule considering geometric adjustment speed	1
Effect of multi-hole arrangement on the effusion cooling with backward injection	1
Deep residual ensemble model for predicting remaining useful life of turbo fan engines	1
Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter	1
Effect of multi-hole arrangement on the effusion cooling with backward injection	1
Investigation of effect of atomization performance on lean blowout limit for gas turbine combustors by comparison of utilizing aviation kerosene and methane as fuel	1
Numerical and experimental study on the critical geometric variation based on sensitivity analysis on a compressor rotor	1
Performance analysis of a gas turbine engine via intercooling and regeneration- Part 2	1
Vortex structure control based bleed in axial compressor cascade with tip clearance using large eddy simulation	1
Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade	1
Performance enhancement and flow separation control in an S-duct by air injection	1
Constant temperature line identification on prototype gas turbine combustor with multi-colour change coating	1
Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field	1
Parametric analysis of thermal cycle of a short take-off and vertical landing engine	1
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser	1
Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification	1