Practical computational fracture mechanics for aircraft structural integrity

Daren Peng; Pu Huang; Rhys Jones

doi:10.1016/B978-0-08-100540-8.00004-2

Practical computational fracture mechanics for aircraft structural integrity

Daren Peng, Pu Huang, Rhys Jones

Mechanical & Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Chapter (Book) › Research › peer-review

6 Citations (Scopus)

Abstract

This chapter presents simple computational tools for determining the stress intensity factors associated with small sub-mm cracks in realistic complex geometries under arbitrary flight loads. Attention is also focused on small initial cracks that first grow as a complex three-dimensional (3D) shape and then transition into a through-the-thickness flaws with an oblique (part) elliptical crack front. Unless otherwise stated these tools are used to perform the lifting and crack growth analyses performed in the various chapters in this book.

Original language	English
Title of host publication	Aircraft Sustainment and Repair
Editors	Rhys Jones, Alan Baker, Neil Matthews, Victor Champagne
Place of Publication	Oxford UK
Publisher	Elsevier
Chapter	4
Pages	67-128
Number of pages	62
Edition	1st
ISBN (Electronic)	9780081005446
ISBN (Print)	9780081005408
DOIs	https://doi.org/10.1016/B978-0-08-100540-8.00004-2
Publication status	Published - 2018

Keywords

3D cracks
Finite boundary modification factor
Finite element analysis
Stress intensity factors

Access to Document

10.1016/B978-0-08-100540-8.00004-2

Cite this

@inbook{6ebd5bdcf0924e02ba2c50aa1eafb986,

title = "Practical computational fracture mechanics for aircraft structural integrity",

abstract = "This chapter presents simple computational tools for determining the stress intensity factors associated with small sub-mm cracks in realistic complex geometries under arbitrary flight loads. Attention is also focused on small initial cracks that first grow as a complex three-dimensional (3D) shape and then transition into a through-the-thickness flaws with an oblique (part) elliptical crack front. Unless otherwise stated these tools are used to perform the lifting and crack growth analyses performed in the various chapters in this book.",

keywords = "3D cracks, Finite boundary modification factor, Finite element analysis, Stress intensity factors",

author = "Daren Peng and Pu Huang and Rhys Jones",

year = "2018",

doi = "10.1016/B978-0-08-100540-8.00004-2",

language = "English",

isbn = "9780081005408",

pages = "67--128",

editor = "Rhys Jones and Alan Baker and Neil Matthews and Victor Champagne",

booktitle = "Aircraft Sustainment and Repair",

publisher = "Elsevier",

address = "Netherlands",

edition = "1st",

}

TY - CHAP

T1 - Practical computational fracture mechanics for aircraft structural integrity

AU - Peng, Daren

AU - Huang, Pu

AU - Jones, Rhys

PY - 2018

Y1 - 2018

N2 - This chapter presents simple computational tools for determining the stress intensity factors associated with small sub-mm cracks in realistic complex geometries under arbitrary flight loads. Attention is also focused on small initial cracks that first grow as a complex three-dimensional (3D) shape and then transition into a through-the-thickness flaws with an oblique (part) elliptical crack front. Unless otherwise stated these tools are used to perform the lifting and crack growth analyses performed in the various chapters in this book.

AB - This chapter presents simple computational tools for determining the stress intensity factors associated with small sub-mm cracks in realistic complex geometries under arbitrary flight loads. Attention is also focused on small initial cracks that first grow as a complex three-dimensional (3D) shape and then transition into a through-the-thickness flaws with an oblique (part) elliptical crack front. Unless otherwise stated these tools are used to perform the lifting and crack growth analyses performed in the various chapters in this book.

KW - 3D cracks

KW - Finite boundary modification factor

KW - Finite element analysis

KW - Stress intensity factors

UR - http://www.scopus.com/inward/record.url?scp=85049012548&partnerID=8YFLogxK

U2 - 10.1016/B978-0-08-100540-8.00004-2

DO - 10.1016/B978-0-08-100540-8.00004-2

M3 - Chapter (Book)

AN - SCOPUS:85049012548

SN - 9780081005408

SP - 67

EP - 128

BT - Aircraft Sustainment and Repair

A2 - Jones, Rhys

A2 - Baker, Alan

A2 - Matthews, Neil

A2 - Champagne, Victor

PB - Elsevier

CY - Oxford UK

ER -

Practical computational fracture mechanics for aircraft structural integrity

Abstract

Keywords

Access to Document

Other files and links

Cite this