Accession Number : AD0761446

Title :   Fatigue Strength of Bolt and Rivet Joints in Airplane Frame,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Nesterenko,G. I.

Report Date : 16 MAY 1973

Pagination or Media Count : 14

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

Descriptors :   (*JOINTS, FATIGUE(MECHANICS)), (*AIRFRAMES, JOINTS), BOLTED JOINTS, RIVETED JOINTS, LOADS(FORCES), STRESSES, FRICTION, USSR

Subject Categories : Aircraft
      Couplers, Fasteners, and Joints

Distribution Statement : APPROVED FOR PUBLIC RELEASE