عنوان

Fatigue crack growth failure and Lifing analyses for metallic aircraft structures and components /

(Number (ISBN

9402416757

(Number (ISBN

9789402416756

Erroneous ISBN

9789402416732

Title Proper

Fatigue crack growth failure and Lifing analyses for metallic aircraft structures and components /

General Material Designation

[Book]

First Statement of Responsibility

Russell Wanhill, Simon Barter, Loris Molent.

Place of Publication, Distribution, etc.

Dordrecht, Netherlands :

Name of Publisher, Distributor, etc.

Springer,

Date of Publication, Distribution, etc.

2019.

Specific Material Designation and Extent of Item

1 online resource (xi, 99 pages) :

Other Physical Details

illustrations (some color)

Series Title

SpringerBriefs in applied sciences and technology,

ISSN of Series

2191-530X

Text of Note

Includes bibliographical references.

Text of Note

Intro; Preface; Contents; Abstract; 1 Historical Review; 1.1 FCG Parameters, Concepts and Testing; 1.2 FCG 'Laws' and Models; 1.2.1 Long Crack Growth 'Laws'; 1.2.2 Long Crack Growth Models: LEFM Analyses; 1.2.3 Characteristic K Approaches; 1.2.4 The Effective Block Approach (EBA) Framework; 1.2.5 Exponential FCG Behaviour; 1.3 Summary; 2 Basic Information for Aircraft FCG Failure and Lifing Analyses; 2.1 Importance of Fatigue for Aircraft Structural Failures; 2.2 Fatigue Crack Nucleation, Discontinuities, Early FCG and Damage Tolerance

Text of Note

2.2.1 Fatigue-Nucleating Discontinuities in Aircraft Structures2.2.2 Early FCG and Damage Tolerance; 2.3 Summary of FCG Lifing Methods; 3 Quantitative Fractography (QF) for FCG Analyses; 3.1 Introduction; 3.2 Fatigue Striation FCG Analyses; 3.3 Progression Marking FCG Analyses; 3.4 Fatigue-Nucleating Discontinuities and Equivalent Pre-crack Sizes (EPS); 3.4.1 Defining the Initial Crack Sizes for FCG Analyses; 3.5 QF Techniques for Fatigue Fracture Surfaces; 3.5.1 Optical Fractography; 3.5.2 Electron Fractography and Optical Fractography; 3.6 A Cautionary Note

Text of Note

4 Aermacchi MB-326H Wing Spar (1990): Exponential FCG Analysis4.1 Introduction; 4.2 FCG Analysis for the Failed Spar; 4.3 Further Examination of Wing Spars; 4.3.1 Safe Life Reassessment; 4.3.2 Fleet Recovery Programme; 4.4 Lessons Learned; 5 P & W 125B Engine Bearing (1994): 2-Stage Exponential FCG Analysis; 5.1 Introduction; 5.2 The Failed No. 3 Bearing: Macroscopic and Metallographic Examination; 5.3 Cage Failure and FCG Analysis; 5.3.1 Progression Marking QF Analysis; 5.4 Interpretation of the Results and Remedial Action

Text of Note

6 EBA Example Lifing Assessment (2004): F/A-18 Horizontal Stabilator Spindles6.1 Introduction; 6.2 EBA Validation for the F/A-18 Horizontal Stabilator Spindles; 6.3 EBA and Total Life Assessment for the F/A-18 Horizontal Stabilator Spindles; 7 LCFLF Example Lifing Assessment (2004): F/A-18 Vertical Tail Attachment Stubs; 7.1 Introduction; 7.2 The FT46 Stub Flange Crack; 7.3 Fractography of the FT46 Stub Flange Crack; 7.4 LCFLF Life Assessment for the FT46 Stub Flange Crack; 8 Cubic Rule Life Prediction Examples; 8.1 Introduction; 8.2 McDonnell Douglas F4E Spectrum Coupon Test Data

Text of Note

8.3 Lockheed Martin P3C Spectrum Coupon Test Data8.4 Summary; 9 Fokker 100 Fuselage Test: Lap Joints Exponential FCG Analysis; 9.1 Introduction; 9.2 FCG Analysis of the Cracked Lap Splice [71, 72, 95]; 10 Sikorsky S-61N Rotor Blade (1974): Exponential FCGR Analysis; 10.1 Introduction; 10.2 FCG Analysis for the Crashed Helicopter; 10.2.1 Prediction of Detectable FCG Lives; 10.3 Results and Remedial Actions (Lessons Learned); 11 Westland Lynx Rotor Hub (1998): Progression Marking LEFM Analysis; 11.1 Introduction; 11.2 Fractography of Early Fatigue Cracking in the M326 'Yellow' Arm

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8

8

8

8

Text of Note

This book provides a concise discussion of fatigue crack growth (FCG) failure and lifing analysis methods for metallic aircraft structures and components. After a reasonably concise historical review, surveys are made of (i) the importance of fatigue for aircraft structural failures and the sources of fatigue nucleation and cracking, (ii) contemporary FCG lifing methods, and (iii) the Quantitative Fractography (QF) required for determining the actual FCG behaviour. These surveys are followed by the main part of the book, which is a discussion, using case histories, of the applicabilities of Linear Elastic Fracture Mechanics (LEFM) and non-LEFM methods for analysing service fatigue failures and full- and sub-scale test results. This discussion is derived primarily from the experiences of the Defence Science and Technology Group in Melbourne, Australia, and the Netherlands Aerospace Centre, Marknesse, the Netherlands.

Source for Acquisition/Subscription Address

Springer Nature

Stock Number

com.springer.onix.9789402416756

International Standard Book Number

9789402416732

International Standard Book Number

9789402416749

Fracture mechanics.

Materials-- Fatigue.

Fracture mechanics.

Materials-- Fatigue.

TEC002000

TRP

TRP

TTDS

Number

Edition

Class number

Wanhill, R. J. H.

Barter, Simon

Molent, Loris

Date of Transaction

20200823215440.0

Cataloguing Rules (Descriptive Conventions))

pn

Electronic name

[Book]

Y