Aeronautical Fatigue Publications and Books:

ICAF 20, 1999 - Structural Integrity for the next Millenium

Proceedings of the 20th Symposium of the International Committee on Aeronautical Fatigue 14-16 July 1999, Bellevue, Washington, USA

VOLUME I

Plantema Memorial Lecture

Advances in Fatigue and Fracture Mechanics Analysis for Aircraft Structures
J NEWMAN Jr

VISIONARY APPROACHES

Effect of Inspection Uncertainty on Aircraft Structural Integrity
J LINCOLN

Corrosion and the Management of Structural Integrity
G CLARK

FATIGUE I

A Practical Engineering Approach to Predicting Fatigue Crack Growth in Riveted Lap Joints
C HARRIS, J NEWMAN Jr, R PIASCIK

Fatigue and Damage Tolerance Design of Large Airbus Wing Structures
E HUNT, M JONES, A WILLIAMS

Stress Intensity Factors and Crack Interaction of Part Elliptical Through Cracks in Adjacent Holes
J J M De RIJCK, J SCHIJVE, A VLOT, S FAWAZ

FATIGUE II

Fatigue Crack Growth and Residual Strength Analysis of Twist Spectrum Loaded Integrally Stiffened Panels Simulating a Lower Wing Skin Two Bay Crack Scenario
M KULAK, R BUCCI, H SKYUT, G BRAY, J NEWMAN Jr

Fatigue and Damage Tolerance Aspects of High Speed Machined Airframe Parts
H ANSELL

WIDESPREAD FATIGUE DAMAGE

A Probabilistic Approach to Predict the Onset of Widespread Fatigue Cracking in Fuselage Structure
R ALFORD, R BELL, S SHAH

An Experimental and Numerical Analysis of Multi-Site Damage Butt-Joints
G CAVALLINI, R GALATOLO, D GUILIANO

Methodologies for the Assessment of Widespread Fatigue Damage in Aircraft Wing Structures
R COLLINS, S KIMMINS

Experimental and Analytical Assessments of Multiple-Site Cracking in Aircraft Fuselage Structure
J BAKACKAS Jr, E AKPAN, C BIGELOW, P TAN

CORROSION/FATIGUE

Stress Corrosion Propagation: Damage Tolerance Approach
D GILLETTA De SAINT-JOSEPH

Review of Pitting Corrosion Fatigue Models
D HOEPPNER, V CHANDRASEKARAN, A M TAYLOR

Corrosion Modeling of KC-135 Lap Joints
R KINZIE, D PEELER, G COOKE

COMPOSITE REPAIR

Issues in the Certification of Bonded Composite Patch Repairs for Cracked Metallic Aircraft Structures
A BAKER

Bonded Composite Repairs for Ageing Commercial Aircraft - A Multi-National Research Effort
A NATHAN

METALLIC REPAIR

Bonded Fiber Metal Laminate Repair Patches
A VLOT, C GUIJT, J GREER, S VERHOEVEN, H WOERDEN

The Evaluation of a Modified Stress Intensity Factor for Cold Expanded Holes
L REID, J RESTIS, T SWIFT

PROBABILISTIC METHODS

Probabilistic Failure Analysis of Fuselage Splice Joints with Multiple Site Fatigue Damage and Corrosion
Y XIONG, G SHI, G SASTAUGH

Fatigue Variability and Life Prediction: A Probabilistic Approach
B HILLBERRY

A Novel Probabilistic Fatigue Crack Growth Solution Based on the Crack Closure Model
G WANG, A BLOM

Probabilities of Occurrence and Detection and Airworthiness Assessment
R WEI, G HARLOW

DAMAGE TOLERANCE

Fractographic Investigation of Pressure Cabin MSD
R WANHILL, W VAN DER HOEVEN, H TEN HOEVE, H OTTENS

Improved Design Criteria for a Large Airbus Aircraft to Meet Future Damage Tolerance Requirements
R BOETSCH, R HEIN, A DAVY

Damage Tolerance Substantiation of the Galaxy Executive Jet
A BROT, S AFNAIM, Z GRANOT

OVERVIEWS

Damage Tolerance in Helicopter Airframes - Is Crack Growth Practical?
M OVERD

Current Status of Research and Development Activities for the Fuselage of a Large Airbus Aircraft
M SCHMIDT, N OHRLOFF, T FLEISCHER

Risk and Economic Implications of DADTA for Foreign Military Operations of Non USAF Fleets
L SCHRADER, O BURNSIDE, J CARDINAL, W SPARKS

EXPERIMENTAL TECHNIQUES

Full Scale Fatigue Test of the Pilatus PC9/A Trainer Aircraft
I ANDERSON, R PARKER

Extended Full-Scale Fatigue Testing of the 777 Fuselage
G DAS, J LUSK, M STARHA

Supplemental Structural Inspection Program and Results for ANA B747SR and B767 Airplanes
K YOSHIOKA, N WAKITA

Results of the DORNIER 328 Operational Loads Recording Campaign
R BRUNBAUER, B HEBING, R TESKE, H HUGH

VOLUME II

POSTER PAPERS

Structural Optimization with Damage Tolerance Constraints
P CHAPERON, J SAWYER, R JONES, F ROSE

Life Extension of an F/A-18 Aileron Hinge Using Structural Optimisation and Bonded Composite Reinforcement
S BAKER, R J CHESTER, M HELLER, S WHITEHEAD, R KAYE, B TEUNISSE

"Of Gnats and Camels" - 30 Years of Regulating Structural Fatigue in Light Aircraft
S SWIFT

The Effect of Peening on the Life Improvement Factor of 7050 AI Alloy Aircraft Structures
K SHARP

Towards a Certification Methodology for Adhesively Bonded Structures and Repairs
M DAVIS

Prediction of the Pitting Behaviour of a Gear Steel
J GUADIN, F CONGOURDEAU, P PEOSSEL

Development of a Test Fixture for Fuselage Curved Panels
M LANGON, C MEYER

Failure Prediction of Aluminium Alloy Stiffened Flat Panels
C SAVES ST GERMES, C MEYER, A DAVY

Modelling of Anisotropy Effects of a Single Crystal Superalloy on its Fatigue-Creep Resistance
F GALLERNEAU

Repeated Load Tests on Airplane with Fiber Composite Structures - Are they Meaningful?
W BROCKER, K WOITHE

Influence of Corrosive Environment on the Fatigue Life of an Ageing Aircraft Structure
G LABEAS, T KERMANIDIS, S PANTELAKIS

Development of a Fatigue-Spectrum for the Nose Landing-Gear Impact on the Galaxy Executive Jet
D CHESTER, A BROT

Fatigue Behaviour of Metallic Lap Joints: A Study of the Effect of Riveting and of the Specimen Geometry
M CHARELLI, A LANCIOTTI, L LAZZERI

Fatigue Crack Growth of a Glare3-5/4 Fiber/Metal Laminate and Validity of Methods for Analysing Results
T SHIMOKAWA, Y KAKUTA, T TAKAMATSU, TM MATSUMURA, N OGURA

Damage Mechanics Approach for Characterisation of Microscopic Fatigue Damage Evolution in Quasi-Isotropic CFRP Laminates
S OGIHARA

Damage Tolerance of Integrally Stiffened and Riveted Stiffened Structures
K G NESTERENKO

Scatter of the Fatigue Life Depleting Process Characteristics
V RACKHER, A NESTEROV, A DOTSENKO, V KONOVALOV

Practical Crack Stopping for Life Enhancement
R COOK

Effect of Shot-Peening on the Fretting Fatigue Behaviour of BS L65 Aluminium Alloy
E DELOSRIOS, M BROWN, A LEVERS, U FERNANDO, E ORLOV

New Progress in Evaluation of Stress Concentration Interactions in the Aerospace Industry
R GRAHAM

Applications of time and Frequency Domain Modelling in Acoustic Fatigue Design
P GREEN

Scatter Considerations in the Interpretation of Major Fatigue Tests
A MEW , A CARDRICK

The Hawk Fatigue Monitoring System
N PENISTONE, L REDMOND

Hawk Structural Life Extension
R SHOOTER

Crack Growth in Stretched Acrylic
S SPENCE

Evaluation and Quantification of Fretting Damage and Corrosion Pit Morphology using the Confocal Microscope
V CHANDRASEKARAN, Y YOON, D HOEPPNER, L GRIMES, A TAYLOR

Quantification and Correlation of Pit Parameters to "Small" Fatigue Cracks
V CHANDRASEKARAN, Y YOON, D HOEPPNER, A TAYLOR

Predicting Component Failure from User-Defined Regime Recognition Data
J CICERO, J MOHAMMADI

A Modern Method for Predicting the Onset of Widespread Fatigue Failure in Aircraft Structure
S FEVOLA

Fretting Crack Nucleation in Riveted Lap Joints - Predictions and Experiments
V G HARISH, T FARRIS, M SZOLWINSKI

Analysis and Observation of Fretting Fatigue of Ti-6AI-4V
G HARISH, P McVEIGH, C TIECHE, T FARRIS, M SZOLWINSKI

Analysis, Design and Test Verification of Composite Reinforcements for Multisite Damage
J HELBLING, M RATWANI

Novel NDE/I Corrosion Rate Measuring System for Airframe Structural Integrity Based on Impedance Spectroscopy
J KIM, A GONZALEZ, D HODKO, W ECKHOFF

Fatigue Crack Growth Prediction for an Advanced Aircraft Structure Using a New Life Prediction Model
M LANG, R DELANEUVILLE, J LARSEN

Mechanical Characterisation of Ceramic Matrix Composite Components
G OJARD, R NAIK, R CAIRO, J HORNICK, G LINSEY, J AMOS, J BRENNAN

Damage Tolerance of Integrally Stiffened Panels - Laboratory Test and Numerical Modeling
J WANG, C HSU, R PETTIT

Empirical Derivation of a Five-Variable Load Spectra from Recorded Data for Aircraft Design and Fatigue Life
J YOST

A Different Perspective of Fundamental Research into Coldworking of Fastener Holes
A LEON

Crack Linkup by Stable Crack Growth
A KOBAYASHI