Designing Turbine Blades for Fatigue and Creep

  • Bruno Dambrine Societe Nationale DEtude Et De Construction De Moteurs DAviations (SNECMA), Paris
  • Jean Pierre Mascarell Societe Nationale DEtude Et De Construction De Moteurs DAviations (SNECMA), Paris
DOI: https://doi.org/10.14429/dsj.38.5872
Keywords: Turbine entry temperature, Cooling technique

Abstract

Abstract not available.

Author Biographies

Bruno Dambrine, Societe Nationale DEtude Et De Construction De Moteurs DAviations (SNECMA), Paris
Societe Nationale DEtude Et De Construction De Moteurs DAviations (SNECMA) 2, Boulevard Victor, 75724  Paris Cedex 15
Jean Pierre Mascarell, Societe Nationale DEtude Et De Construction De Moteurs DAviations (SNECMA), Paris
Societe Nationale DEtude Et De Construction De Moteurs DAviations (SNECMA) 2, Boulevard Victor, 75724  Paris Cedex 15
Published
2014-01-13
How to Cite
Dambrine, B., & Mascarell, J. (2014). Designing Turbine Blades for Fatigue and Creep. Defence Science Journal, 38(4), 413-430. https://doi.org/10.14429/dsj.38.5872
Issue
Vol 38 No 4
Section
General Papers
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