Journal of Turbomachinery-Transactions of the Asme

Papers
(The H4-Index of Journal of Turbomachinery-Transactions of the Asme is 16. 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.)
ArticleCitations
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics43
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method32
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions32
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise26
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition26
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions24
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound24
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating23
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow21
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade19
Exploring Topology Optimization for High Pressure Turbine Blade Tips18
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade18
Performance Sensitivity of a Grooved Tip Seal to Manufacturing and Operational Geometry Deviations18
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness17
Reviewer’s Recognition17
Evaluation of Cooling Requirements for Rotating Detonation Combustors17
Nonlinear Flutter Analysis of Labyrinth Seals16
A New Multi-Stage Turbine Stator Design for Improved Performance Retention16
A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation16
Roughness Investigations on In-Service High-Pressure Compressor Blades—Part II: Roughness Parameterization and Computational Fluid Dynamics-Based Modeling of Its Impact on Turbulent Flows16
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