Stress-Intensity Factor Solutions for Cracks at Countersunk Rivet Holes Under Uniaxial Tension

Tan, P W; Bigelow, C A; O'Donoghue, P. E.; Atluri, S. N.

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Stress-Intensity Factor Solutions for Cracks at Countersunk Rivet Holes Under Uniaxial Tension

1994-02-01
By Tan, P W ; Bigelow, C A ; O'Donoghue, P. E.

File Language:

English

Details

Creators:

Tan, P W ; Bigelow, C A ; O'Donoghue, P. E. ; Atluri, S. N.
Corporate Creators:

United States. Department of Transportation. Federal Aviation Administration. Technical Center
Subject/TRT Terms:
Publication/ Report Number:

DOT/FAA/CT-93/68
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
Abstract:

To predict crack growth and fracture strengths of riveted joints subjected to widespread fatigue damage, accurate stress and fracture analyses of corner and surface cracks at a rivet hole are needed. The results presented in this report focus on the computation of stress-intensity factor solutions for rivet holes with cracks. The stress-intensity factor solutions for surface and corner cracks at countersunk rivet holes in a plate were obtained using the finite-element-alternating technique. A range of crack shapes, crack sizes, and crack locations under remote tension were considered.
Format:

PDF
Download URL:

https://rosap.ntl.bts.gov/view/dot/93448/dot_93448_DS1.pdf
File Type:

[PDF - 553.81 KB]
Collection(s):

FAA William J. Hughes Technical Center for Advanced Aerospace
Main Document Checksum:

urn:sha-512:7e6e4b9f58351f20385ee3025d8aaae2ac9d9347fdee33b34ca637499a8a4ac006eff68b023955d4917c21618eaf8c519ff5d2f7733adfc5560fe4dce7bcdbcd

File Language:

English

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