World's Best Scientists 2026 revealed!

D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
30
Citations
2953
World Ranking
3423
National Ranking
26

Research.com Recognitions

  • 2000 - Fellow of the American Society of Mechanical Engineers

Best Publications

  • An Experimental and Numerical Investigation Into the Mechanisms of Rotating Instability

    Unknown

  • Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor: Criteria and Mechanisms

    Unknown

  • Development of Hub Corner Stall and Its Influence on the Performance of Axial Compressor Blade Rows

    Unknown

  • Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor

    Unknown

  • A Navier-Stokes Analysis of Three-Dimensional Turbulent Flows Inside Turbine Blade Rows at Design and Off-Design Conditions

    Unknown

  • Turbine Tip and Shroud Heat Transfer

    D. E. Metzger;M. G. Dunn;C. Hah

  • Application of Casing Circumferential Grooves for Improved Stall Margin in a Transonic Axial Compressor

    Unknown

  • Role of Tip-Leakage Vortices and Passage Shock in Stall Inception in a Swept Transonic Compressor Rotor

    Unknown

  • Development of Hub Corner Stall and Its Influence on the Performance of Axial Compressor Blade Rows

    Unknown

  • Control of Shock Structure and Secondary Flow Field Inside Transonic Compressor Rotors Through Aerodynamic Sweep

    Unknown

  • Effect of Circumferential Grooves on the Aerodynamic Performance of an Axial Single-Stage Transonic Compressor

    Unknown

  • Measurement and prediction of mean velocity and turbulence structure in the near wake of an airfoil

    Unknown

  • Turbine Tip and Shroud Heat Transfer

    Unknown

  • Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades

    Unknown

  • The Effect of Tip Clearance on a Swept Transonic Compressor Rotor

    Unknown

  • Secondary Flows and Vortex Motion in a High-Efficiency Backswept Impeller at Design and Off-Design Conditions

    Unknown

  • A Numerical Modeling of Endwall and Tip-Clearance Flow of an Isolated Compressor Rotor

    Unknown

  • Large Eddy Simulation of Transonic Flow Field in NASA Rotor 37

    Unknown

  • INVESTIGATION OF PASSAGE FLOW FEATURES IN A TRANSONIC COMPRESSOR ROTOR WITH CASING TREATMENTS

    Unknown

  • Tip Clearance Vortex Oscillation, Vortex Shedding and Rotating Instabilities in an Axial Transonic Compressor Rotor

    Unknown

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