Accession Number:

ADA955618

Title:

Applicability of Fracture Mechanics to Aircraft Engine Disc Low Cycle Fatigue Life.

Descriptive Note:

Final rept. 1 Jun 74-30 Sep 75,

Corporate Author:

VANDERBILT UNIV NASHVILLE TN DEPT OF MATERIALS SCIENCE

Personal Author(s):

Report Date:

1977-04-01

Pagination or Media Count:

93.0

Abstract:

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE