World's Best Scientists 2026 revealed!

D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
34
Citations
5798
World Ranking
2798
National Ranking
203

Research.com Recognitions

  • 2000 - Fellow of the Royal Society, United Kingdom
  • 1993 - Fellow of the Royal Academy of Engineering (UK)

Best Publications

  • The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines

    Unknown

  • Loss Mechanisms in Turbomachines

    Unknown

  • The Calculation of Three-Dimensional Viscous Flow Through Multistage Turbomachines

    Unknown

  • Development of Blade Profiles for Low-Pressure Turbine Applications

    E. M. Curtis;H. P. Hodson;M. R. Banieghbal;J. D. Denton

  • An Improved Time-Marching Method for Turbomachinery Flow Calculation

    Unknown

  • Some Limitations of Turbomachinery CFD

    Unknown

  • Throughflow Calculations for Transonic Axial Flow Turbines

    Unknown

  • Computational fluid dynamics for turbomachinery design

    Unknown

  • The Effects of Lean and Sweep on Transonic Fan Performance

    Unknown

  • Lessons from rotor 37

    Unknown

  • The exploitation of three-dimensional flow in turbomachinery design

    Unknown

  • Blade-Row Interaction in a High-Pressure Turbine

    V. S. P. Chaluvadi;A. I. Kalfas;M. R. Banieghbal;H. P. Hodson

  • A Review of Some Early Design Practice Using Computational Fluid Dynamics and a Current Perspective

    Unknown

  • The Trailing Edge Loss of Transonic Turbine Blades

    Unknown

  • Three-Dimensional Time-Marching Inviscid and Viscous Solutions for Unsteady Flows Around Vibrating Blades

    Unknown

  • The Use of a Distributed Body Force to Simulate Viscous Effects in 3D Flow Calculations

    Unknown

  • A Numerical Investigation Into the Sources of Endwall Loss in Axial Flow Turbines

    Unknown

  • A time marching method for two-and three-dimensional blade to blade flows

    Unknown

  • An Improved Time Marching Method for Turbomachinery Flow Calculation

    Unknown

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

    Unknown

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