OOIR: Observatory of International Research

Papers

(The TQCC of International Journal of Turbo & Jet-Engines is 2. 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 2021-11-01 to 2025-11-01.)

Article	Citations
Frontmatter	36
Frontmatter	18
Design optimization of a fluidic thrust vectoring system based on coanda effect using meta-models	14
Numerical study of transition process in different zones of a compressor cascade channel	10
Uncertainty propagation in transient heat transfer from an extended surface	9
Performance enhancement and flow separation control in an S-duct by air injection	8
Endwall-pulsed blowing of different excitation models to control flow separation on a highly-loaded compressor cascade	8
Role of different cavity flame holders on the performance characteristics of supersonic combustor	8
Research on real-time improvement method of on-board physical mechanism model of turboshaft engine based on neural network	8
Active subspace-based performance analysis of supersonic through-flow fan rotor	7
Application of KH-RT model in lifting flame of methanol jet atomization	7
Frontmatter	7
Detailed investigation of supersonic film cooling performance in a convergent divergent nozzle	6
Study of a new effervescent atomizer design	6
C conjugate heat transfer simulation of swirl internal cooling on blade leading edge	6
Investigations of modified cooling hole injection angle configurations for improved trench film cooling performance	6
Control of subsonic jets using vanes as vortex generators	5
Numerical study of effect of the casing slot on the tip leakage vortex and vortex cavitation of a fuel pump	5
Performance analysis of a gas turbine engine with intercooling and regeneration process - Part 1	5
Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters	5
Frontmatter	5
Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan	4
A new schedule method for compact propulsion system model	4
Influence mechanism of advance ratio on the aerodynamic performance of a contra-rotating propfan	4
Research on adjoint-based customized integrated passage design of Rotor 67	4

Frontmatter	4
Computational analysis of the scramjet mode of the RBCC inlet using micro vortex generators	4
Research on high-bandwidth linear active disturbance rejection control method for variable speed turboshaft engine	4
A cooled turbine airfoil performance prediction method with two-dimensional CFD computation and loss models	4
Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence	4
Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis	4
Influences of unbalance phase combination on the dynamic characteristics for a turboprop engine	3
Research on turboprop engine control method based on linear parameter varying model	3
Study on laser de-weight and dynamic balance technology of rotating machines	3
Aerothermal effects of squealer openings on a cavity tip in a turbine cascade	3
Simulation and analysis of the over-expanded flow field in asymmetric nozzles with lateral expansion	3
Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification	3
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity	3
Influence of non-axisymmetric endwall profiling under incoming vortex on the corner separation of a diffusion cascade	3
Optimization-based transient control of turbofan engines: a sequential quadratic programming approach	3
Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall	2
Air tab location effect on supersonic jet mixing	2
A novel degradation estimation of lifecycle health monitoring for aircraft engine gas path rotational components	2
Turbojet module sizing for integration with turbine-based combined cycle engine	2
Modeling and analysis of 3D radiative heat transfer in combustor	2
Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity	2
Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties	2
Effect of free boundary on the performance of single expansion nozzle	2
An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil	2
A torsional vibration coupling dynamic modeling and analysis method for engine/power transmission systems in coaxial high-speed helicopters	2
Infrared simulation of aircraft rear fuselage based on a coupled CFD method	2
Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage	2
Performance analysis of a planar shaped strut injector based supersonic combustion chamber	2
Design and analysis of air intake of subsonic cruise vehicle with experimental validation	2
Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine	2
Numerical investigation on mixing of heated confined swirling coaxial jets with blockage	2
Numerical investigation of ice crystal melting characteristic and icing risk in an axial compressor	2
Influence of conical shaft stiffness on the dynamic characteristics of flexible rotor	2
Numerical investigation of a novel mushroom-shaped cooling hole for enhanced film cooling performance	2
Exergy Analysis of a Turboprop Engine at Different Flight Altitude and Speeds Using Novel Consideration	2
Study of vortex throttle characteristics with adjustable resistance by rotation of the vortex chamber inlet channel	2
Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions	2
Integration of multi module flow domain to demonstrate the full engine aero-flow path simulation of Single Spool Turbojet Engine	2