Accession Number:

AD0756893

Title:

Composite Wing for Transonic Improvement, Volume 3. Structural Reliability Studies

Descriptive Note:

Final technical rept.

Corporate Author:

GENERAL DYNAMICS FORT WORTH TX CONVAIR AEROSPACE DIV

Report Date:

1972-11-01

Pagination or Media Count:

245.0

Abstract:

A discussion is presented on the development of a reliability based technology for the design of large scale bonded joints and on the development of a data base, using boron epoxy to titanium double scarf bonded joint specimens to explore the character of the failure process and to determine the joint characteristics which effect structural reliability.

Subject Categories:

  • Aircraft
  • Couplers, Fasteners and Joints

Distribution Statement:

APPROVED FOR PUBLIC RELEASE