World's Best Scientists 2026 revealed!

D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
30
Citations
3469
World Ranking
3397
National Ranking
246

Best Publications

  • Finite element model updating using frequency response function data: I. Theory and initial investigation

    M. Imregun;W.J. Visser;D.J. Ewins

  • STRUCTURAL DAMAGE DETECTION USING ARTIFICIAL NEURAL NETWORKS AND MEASURED FRF DATA REDUCED VIA PRINCIPAL COMPONENT PROJECTION

    Unknown

  • Structural Damage Detection using Independent Component Analysis

    C. Zang;M. I. Friswell;M. Imregun

  • Harmonic Balance Vibration Analysis of Turbine Blades With Friction Dampers

    K. Y. Sanliturk;M. Imregun;D. J. Ewins

  • A REVIEW OF AEROELASTICITY METHODS WITH EMPHASIS ON TURBOMACHINERY APPLICATIONS

    Unknown

  • An improved single-parameter tip-timing method for turbomachinery blade vibration measurements using optical laser probes

    Unknown

  • A Survey of Blade Tip-Timing Measurement Techniques for Turbomachinery Vibration

    Unknown

  • Modeling of Three-Dimensional Viscous Compressible Turbomachinery Flows Using Unstructured Hybrid Grids

    Unknown

  • Technical Article: practical articles in shock and vibration technology

    Unknown

  • On the Use of Atmospheric Boundary Conditions for Axial-Flow Compressor Stall Simulations

    Unknown

  • Finite element model updating using frequency response function data. II. Case study on a medium-size finite element model

    M. Imregun;K.Y. Sanliturk;D.J. Ewins

  • Forced harmonic response analysis of nonlinear structures using describing functions

    Unknown

  • AN INTEGRATED NONLINEAR APPROACH FOR TURBOMACHINERY FORCED RESPONSE PREDICTION. PART I: FORMULATION

    Unknown

  • Mechanisms for Wide-Chord Fan Blade Flutter

    Unknown

  • Mechanisms and Prediction Methods for Fan Blade Stall Flutter

    Unknown

  • AN INTEGRATED NONLINEAR APPROACH FOR TURBOMACHINERY FORCED RESPONSE PREDICTION. PART II: CASE STUDIES

    Unknown

  • Combined neural network and reduced FRF techniques for slight damage detection using measured response data

    Unknown

  • FREQUENCY–DOMAIN CRITERIA FOR CORRELATING AND UPDATING DYNAMIC FINITE ELEMENT MODELS

    Unknown

  • Effects of Fan Speed on Rotating Stall Inception and Recovery

    Unknown

  • Unsteady Flow and Aeroelasticity Behavior of Aeroengine Core Compressors During Rotating Stall and Surge

    Unknown

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