Stress-Intensity Factors along Three-Dimensional Elliptical Crack Fronts

Gosz, M.; Moran, B.

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Stress-Intensity Factors along Three-Dimensional Elliptical Crack Fronts

1998-05-01
By Gosz, M. ; Moran, B.

File Language:

English

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Creators:

Gosz, M. ; Moran, B.
Corporate Creators:

University of New Hampshire. Dept. of Mechanical Engineering ; Northwestern University (Evanston, Ill.). Center for Quality Engineering and Failure Prevention
Corporate Contributors:

United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research
Subject/TRT Terms:

Crack And Seat Treatment Elliptical Crack Fronts Finite Element Method Fracture Properties Integral Equations Modulus Of Elasticity Poisson Ratio Stress Intensity Factors Structural Analysis Three-dimensional
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration
Abstract:

The objective of the present investigation is to determine the mode I stress-intensity factors along two symmetric surface cracks emanating from a centrally located hole in a rectangular plate (the so-called Round Robin Problem) using the domain integral. See also PB98-146186. Prepared in cooperation with Northwestern Univ., Evanston, IL. Center for Quality Engineering and Failure Prevention. Sponsored by Federal Aviation Administration, Washington, DC. Office of Aviation Research.
Format:

PDF
Collection(s):

US Transportation Collection
Main Document Checksum:

urn:sha-512:c0d0818ed0eddea53bcae8bd41098c06a26292f3bc892fd9a5456ac25d8896f94411dfc7da3e07593e8e35816b74da01266d84b75068b3888cc6406b6d488f25
Download URL:

https://rosap.ntl.bts.gov/view/dot/36199/dot_36199_DS1.pdf
File Type:

[PDF - 575.20 KB ]

File Language:

English

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