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Thermal Barrier Coating (TBC) Failure Modes

The Defense Systems Information Analysis Center (DSIAC) was asked to collect information and limited distribution reports on the failure modes and causes for failure of TBCs used in military aircraft turbine engines. It was determined…

Ceramic Additive Manufacturing for Gas Turbine Engine Blades

  The Defense Systems Information Analysis Center (DSIAC) received a technical inquiry requesting information on current research, development, testing, and evaluation (RDT&E) efforts on ceramic additively manufactured (AM) gas engine turbine blades. DSIAC staff contacted subject matter…

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