World's Best Scientists 2026 revealed!

D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
33
Citations
5414
World Ranking
2980
National Ranking
36

Best Publications

  • Internal Flow: Concepts and Applications

    Edward M. Greitzer;Choon Sooi Tan;Martin B. Graf

  • Criteria for Spike Initiated Rotating Stall

    Huu Duc Vo;Choon S. Tan;Edward M. Greitzer

  • Role of Blade Passage Flow Structurs in Axial Compressor Rotating Stall Inception

    Donald A.Hoying;Choon S.Tan;Huu Duc Vo;Edward M.Greitzer

  • Endwall Blockage in Axial Compressors

    S. A. Khalid;A. S. Khalsa;I. A. Waitz;C. S. Tan

  • Spike-Type Compressor Stall Inception, Detection, and Control

    C.S. Tan;I. Day;S. Morris;A. Wadia

  • Similarity analysis of compressor tip clearance flow structure

    G. T. Chen;E. M. Greitzer;C. S. Tan;F. E. Marble

  • Internal Flow

    Unknown

  • A Computational Model for Short-Wavelength Stall Inception and Development in Multistage Compressors

    Unknown

  • Enhanced mixing with streamwise vorticity

    I.A. Waitz;Y.J. Qiu;T.A. Manning;A.K.S. Fung

  • Mechanisms of inlet-vortex formation

    F. De Siervi;H. C. Viguier;E. M. Greitzer;C. S. Tan

  • Numerical simulation of compressor endwall and casing treatment flow phenomena

    A. J. Crook;E. M. Greitzer;C. S. Tan;J. J. Adamczyk

  • Analysis of Fan Stage Conceptual Design Attributes for Boundary Layer Ingestion

    David K. Hall;Edward M. Greitzer;Choon S. Tan

  • Active Control of Tip Clearance Flow in Axial Compressors

    Jin Woo Bae;Kenneth S. Breuer;Choon S. Tan

  • Impeller–Diffuser Interaction in a Centrifugal Compressor

    Unknown

  • Effects of rotating inlet distortion on multistage compressor stability

    J. P. Longley;H. W. Shin;R. E. Plumley;P. D. Silkowski

  • Compressor Efficiency Variation With Rotor Tip Gap From Vanishing to Large Clearance

    Unknown

  • Theory of Blade Design for Large Deflections: Part I—Two-Dimensional Cascade

    Unknown

  • Effects of Non-Axisymmetric Tip Clearance on Axial Compressor Performance and Stability

    M. B. Graf;T. S. Wong;E. M. Greitzer;F. E. Marble

  • Turbine Hub and Shroud Sealing Flow Loss Mechanisms

    Unknown

  • N+3 Aircraft Concept Designs and Trade Studies. Volume 1

    E. M. Greitzer;P. A. Bonnefoy;E. DelaRosaBlanco;C. S. Dorbian

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