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Multi-blade shedding in turbines with different casing and blade tip architectures

  • Published:2019-04 Issue: Volume:87 Page:300-310
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Eryilmaz IbrahimORCID,Guenchi Biläl,Pachidis Vassilios

Funder

Rolls-Royce plc

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Development of an Advanced Fan Blade Containment System;Lane,1989

2. The impact load on containment rings during a multiple blade shed in aircraft gas turbine engines;Dewhurst,1991

3. Perforation of aero-engine fan casing by a single rotating blade;He;Aerosp. Sci. Technol.,2013

4. Containment and penetration simulation in case of blade loss in a low pressure turbine;Kraus,2002

5. Blade impact simulation against turbine casings;Hermosilla,2004

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