ISSN: 0889-504X

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Journal of Turbomachinery Q1 Unclaimed

The American Society of Mechanical Engineers(ASME) United States

Unfortunately this journal has not been claimed yet. For this reason, some information may be unavailable.

Journal of Turbomachinery is a journal indexed in SJR in Mechanical Engineering with an H index of 122. It has an SJR impact factor of 0,824 and it has a best quartile of Q1. It is published in English. It has an SJR impact factor of 0,824.

Type: Journal

Type of Copyright:

Languages: English

Open Access Policy:

Type of publications:

Publication frecuency: -

Categories: Mechanical Engineering (Q1)

Price

- €

Inmediate OA

NPD

Embargoed OA

- €

Non OA

Metrics

0,824

SJR Impact factor

122

H Index

165

Total Docs (Last Year)

428

Total Docs (3 years)

4754

Total Refs

1345

Total Cites (3 years)

426

Citable Docs (3 years)

2.74

Cites/Doc (2 years)

28.81

Ref/Doc

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Aims and Scope

Best articles by citations

Separated Flow Transition Under Simulated Low-Pressure Turbine Airfoil Conditions - Part 1: Mean Flow and Turbulence Statistics

Separated Flow Transition Under Simulated Low-Pressure Turbine Airfoil Conditions - Part 2: Turbulence Spectra

Reduction of Secondary Flow Losses in Turbine Cascades by Leading Edge Modifications at the Endwall

Correlation of Film-Cooling Effectiveness From Thermographic Measurements at Enginelike Conditions

Thermomechanical Analysis of Transient Temperatures in a Radial Turbine Wheel

Simulations of the Unsteady Flow Through the Fastrac Supersonic Turbine

Impeller-Diffuser Interaction in a Centrifugal Compressor

A Transport Model for the Deterministic Stresses Associated With Turbomachinery Blade Row Interactions

The Control of Shroud Leakage Flows to Reduce Aerodynamic Losses in a Low Aspect Ratio, Shrouded Axial Flow Turbine

Experimental and Computational Study of the Effect of Momentum-Flux Ratio on High-Pressure Nozzle Guide Vane Endwall Cooling Systems

Influence of Surface Roughness on Heat Transfer and Effectiveness for a Fully Film Cooled Nozzle Guide Vane Measured by Wide Band Liquid Crystals and Direct Heat Flux Gages

Heat Transfer Coefficients and Film Cooling Effectiveness on the Squealer Tip of a Gas Turbine Blade

SHOW MORE ARTICLES

The Effects of Radially Distorted Incident Flow on Performance of Axial-Flow Fans With Forward-Skewed Blades

Analysis of Rotor-Rotor and Stator-Stator Interferences in Multi-Stage Turbomachines

The Use of Hot-Wire Anemometry to Investigate Unsteady Wake-Induced Boundary-Layer Development on a High-Lift LP Turbine Cascade

Transient Thermal Field Measurements in a High Aspect Ratio Channel Related to Transient Thermochromic Liquid Crystal Experiments

Combined 3-D Flow and Heat Transfer Measurements in a 2-Pass Internal Coolant Passage of Gas Turbine Airfoils

Influence of Injection Type and Feed Arrangement on Flow and Heat Transfer in an Injection Slot

Measurements in a Turbine Cascade Flow Under Ultra Low Reynolds Number Conditions

Quantitative Computational Fluid Dynamics Analyses of Particle Deposition on a Transonic Axial Compressor Blade - Part I: Particle Zones Impact

Implementation of a Compressor Face Boundary Condition Based on Small Disturbances

Porosity-Driven Approaches to Model Fouling Effects on Flow Field

A Study of the Effects of Tip Clearance in a Supersonic Turbine

Axial Compressor Deterioration Caused by Saltwater Ingestion