Journal of Turbomachinery-Transactions of the Asme

Papers
(The H4-Index of Journal of Turbomachinery-Transactions of the Asme is 19. 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 2022-08-01 to 2026-08-01.)
ArticleCitations
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions59
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow43
Performance Sensitivity of a Grooved Tip Seal to Manufacturing and Operational Geometry Deviations37
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method34
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness30
Evaluation of Cooling Requirements for Rotating Detonation Combustors29
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound28
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade26
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade24
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics23
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise23
Reviewer’s Recognition21
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions21
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition21
Nonlinear Flutter Analysis of Labyrinth Seals21
An Exception Algorithm to Ease Convergence in Multistage Turbomachinery Throughflow Calculations21
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor20
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage20
Effects of Blade Solidity and Aspect Ratio on a 0.5 Hub-to-Tip Ratio Tube-Axial Fan20
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