Designing Turbine Blades for Fatigue and Creep

Authors

  • 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

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Published

2014-01-13

How to Cite

Dambrine, B., & Mascarell, J. P. (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

License

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