Accession Number:

AD1161002

Title:

Damage Progression in Generic Ceramic Matrix Composite Turbine Airfoils

Descriptive Note:

[Technical Report, Final Report]

Corporate Author:

ARCTOSAIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OHDAYTON UNIV OH

Report Date:

2022-01-31

Pagination or Media Count:

116

Abstract:

A dedicated experimental test program was conducted to characterize the development of damage in generic airfoils manufactured using ceramic matrix composites and to compare those results to FEA predictions. This report describes test results for interlaminar tension, tensile in-plane shear, tensile, fatigue, creep rupture, and subelement testing.

Subject Categories:

  • Mechanics
  • Ceramics, Refractories and Glass
  • Mechanics
  • Ceramics, Refractories and Glass

Distribution Statement:

[A, Approved For Public Release]