INVESTIGATION OF THE FATIGUE CRACK GROWTH CHARACTERISTICS OF Ti-17

Authors
  1. McCammond, D.
  2. Nummi, M.
Corporate Authors
Defence Research Establishment Pacific, Victoria BC (CAN);Toronto Univ, Toronto ONT (CAN) Dept of Mechanical Engineering
Abstract
The report summarizes test results of fatigue crack growth rate experiments on corner crack specimens taken from a Ti-17 compressor disc forging. The data forms part of the Canadian contribution to the AGARD Structures and Materials Panel Program on damage tolerance of gas turbine engine discs.
Report Number
DREP-CRS-89-32 — Contractors Report Series
Date of publication
15 Jun 1989
Number of Pages
127
DSTKIM No
89-03852
CANDIS No
61746
Format(s):
Hardcopy;Originator's fiche received by DSIS

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