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 2021-06-01 to 2025-06-01.)
ArticleCitations
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating31
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness29
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition24
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions23
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise22
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
Experimental and Numerical Study of an Open Impeller Centrifugal Compressor Stage Utilizing Three-Dimensional (3D) Diffuser End Wall Contouring for Operating Range Extension20
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound19
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade19
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade19
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics18
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions17
Evaluation of Cooling Requirements for Rotating Detonation Combustors17
Exploring Topology Optimization for High Pressure Turbine Blade Tips17
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage16
Coupled Time and Passage Spectral Method for an Efficient Resolution of Turbomachinery Far Upstream Wakes16
0.19973802566528