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Email

massimiliano.nardini@unimelb.edu.au

Credentials


Position
Honorary (Fellow)
Department of Mechanical Engineering
Education
PhD
University of Melbourne
Masters
University of Pisa
Bachelors Degree
University of Pisa
ORCID

0000-0002-3023-9069

Dr Massimiliano Nardini

Honorary (Fellow)
Department of Mechanical Engineering

33 Scholarly works
0 Projects

HIGHLIGHTS

  • 2025

    Journal article

    Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024-122305)
    DOI: 10.1115/1.4067442
  • 2025

    Journal article

    Effects of Localized Non-Gaussian Roughness on High-Pressure Turbine Aerothermal Performance: Convective Heat Transfer, Skin Friction, and the Reynolds' Analogy
    DOI: 10.1115/1.4067354
  • 2025

    Journal article

    Performance of Rough-Ribbed Low-Pressure Turbine Blades Under Varying Loading and Operating Conditions
    DOI: 10.1115/1.4066815
  • 2024

    Journal article

    Direct Numerical Simulation of Transitional and Turbulent Flows Over Multi-Scale Surface Roughness—Part II: The Effect of Roughness on the Performance of a High-Pressure Turbine Blade
    DOI: 10.1115/1.4063974
  • 2024

    Journal article

    Effects of Riblet Dimensions on the Transitional Boundary Layers Over High-Lift Turbine Blades
    DOI: 10.1115/1.4064087
  • 2024

    Journal article

    Direct Numerical Simulation of Transitional and Turbulent Flows Over Multi-Scale Surface Roughness—Part I: Methodology and Challenges
    DOI: 10.1115/1.4063753
  • 2024

    Conference Proceedings

    DNS OF TURBINE VANES SUBJECTED TO INLET TEMPERATURE VARIATIONS AND ROBUST QUANTIFICATION OF AEROTHERMAL FLOW IRREVERSIBILITIES
    DOI: 10.1115/GT2024-126865
Massimiliano Nardini

RECENT SCHOLARLY WORKS

  • 2024

    Conference Proceedings

    PERFORMANCE OF ROUGH-RIBBED LOW-PRESSURE TURBINE BLADES UNDER VARYING LOADING AND OPERATING CONDITIONS
    DOI: 10.1115/GT2024-127998
  • 2024

    Conference Proceedings

    Direct Numerical Simulation of the Acoustic Response of a NACA-0012 Airfoil with an Elastic Serrated Trailing-Edge
    DOI: 10.2514/6.2024-3364
  • 2024

    Conference Proceedings

    OPTIMAL RIBLETS APPLIED TO GAS TURBINE COMPRESSOR BLADES STUDIED VIA DIRECT NUMERICAL SIMULATION
    DOI: 10.1115/GT2024-122305

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