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  • About us
    • About us
    • Scope
    • Statute
    • E-CAero2 project
    • Associated organisations
  • Events
    • Conferences
      • New conference: ETC16
      • About conferences
        • About conferences
        • Scope of conferences
        • Reviewing policy
      • Past conferences
        • All past conferences
        • ETC15 – 2023
        • ETC14 – 2021
        • ETC13 – 2019
        • ETC12 – 2017
        • ETC11 – 2015
        • ETC10 – 2013
        • ETC09 – 2011
  • Publications
    • Welcome page
    • Conference Proceedings Repository
      • General repository
      • All papers
      • Invited Lecturers
      • ETC15 / 2023
      • ETC14 / 2021
      • ETC13 / 2019
      • ETC12 / 2017
      • ETC11 / 2015
      • ETC10 / 2013
    • The International Journal of Turbomachinery Propulsion and Power
    • Publication ethics policy
      • Foreword
      • Amending Published Material Policy
      • Dissemination Ethics
      • Copyrights and Licensing
    • ETC Copyright agreement
  • Submission area
    • Guidelines for Authors
      • Guidelines for Authors
      • Preparing the full paper
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      • Abstract submission – pdf
    • Guidelines for Reviewers
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Tag Archives: AXIAL COMPRESSORS

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  2. Paper

Thermal Endwall Effects on Spanwise Mixing in a High-Speed, Multi-Stage Axial Compressor

By Francesco Schinaia2023-11-29Leave a comment

Vortex lattice method for fan tip-flow modeling

By Francesco Schinaia2023-11-29Leave a comment

Assessment of geometrical variability effects through a viscous through-flow model: sensitivity analysis of geometrical variabilities on performance of axial-flow compressor blades

By Francesco Schinaia2023-11-29Leave a comment

Steady and Unsteady Numerical Characterisation of the Secondary Flow Structures of a Highly-Loaded Low-Pressure Compressor Stage

By Francesco Schinaia2023-11-29Leave a comment

Low Reynolds Number Effect on Highly Loaded Compressor Stator Cascade

By Francesco Schinaia2023-11-29Leave a comment

The Current Gap Between Design Optimization and Experiments for Transonic Compressor Blades

By Francesco Schinaia2023-11-29Leave a comment

Investigation on the effects of blade leading-edge protuberances on the aerodynamic performance of an axial transonic compressor

By Francesco Schinaia2023-11-29Leave a comment

Effect of tip gap size on the performance of an axial compressor stage with and without active flow control.

By Francesco Schinaia2023-11-29Leave a comment

Effect of leading edge erosion on the performance of transonic compressor blades

By Francesco Schinaia2023-11-29Leave a comment

Exergetic analysis of the nasa rotor 37 compressor test case

By Francesco Schinaia2023-11-29Leave a comment
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