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 2021-08-01 to 2025-08-01.)
ArticleCitations
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise34
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition32
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade29
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound27
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade23
Coupled Time and Passage Spectral Method for an Efficient Resolution of Turbomachinery Far Upstream Wakes22
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics22
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions21
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method20
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow20
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness19
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions18
Exploring Topology Optimization for High Pressure Turbine Blade Tips18
Evaluation of Cooling Requirements for Rotating Detonation Combustors17
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating16
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
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors16
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