Accession Number:

AD0761446

Title:

Fatigue Strength of Bolt and Rivet Joints in Airplane Frame,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1973-05-16

Pagination or Media Count:

14.0

Abstract:

The author examined the effect of friction forces on the nature of fatigue breakdown of bolt and rivet joints in aircraft structures.

Subject Categories:

  • Aircraft
  • Couplers, Fasteners and Joints

Distribution Statement:

APPROVED FOR PUBLIC RELEASE