Aeronautical Fatigue Publications and Books:

ICAF 19, 1997 - Fatigue in New and Ageing Aircraft

Proceedings of the 19th Symposium of the International Committee on Aeronautical Fatigue 18-20 June 1997, Edinburgh, Scotland

VOLUME I

Plantema Memorial Lecture

Ageing Aircraft USAF Experience and Actions
JOHN W LINCOLN

Recovery of the RAAF Macchi MB326H - The Tale of an Ageing Trainer Fleet
G CLARK, G S JOST, G D YOUNG

The Alphajet Life Extention Program
L DEFEVER, T COURBE, L LE TELLIER

Concorde Structural Relife
A JEFFERSON, P DELORME

The Characteristics of Multi-Site Fatigue Damage in the Fuselage Riveted Lap Splice Joint
R S PIASCIK, S A WILLARD

Analysis of the Formation and Propagation of Widespread Fatigue Damage
A F GRANDT Jr, T N FARRIS, B M HILLBERRY

Numerical 'Round Robin' Tests on the Assessment of MSD
P HORST, GARTEUR ACTION GROUP

Te* as a Low-Cycle Fatigue Crack Growth Parameter -
M T KOKALY, Y OMORI, A S KOBAYASHI, S N ATLURI, P W TAN

A Monte-Carlo Approach for the Assessment of Widespread Fatigue Damage in Aircraft Structures
A SANTGERMA, J GUILLOT, M BALZANO

Bulging Factors for Predicting Residual Strength of Fuselage Panels
J G BUKUCKAS JR, P V NGUYEN, C A BIGELOW, D BROEK

Probability Modelling of Corrosion Fatigue Crack Growth and Pitting Corrosion
R P WIE, C LI, D G HARLOW, T H FLOURNOY

Corrosion/Fatigue Metrics
R PEREZ

Fatigue Strength of Fuselage Joint Structures under Ambient and Corrosive Environment
S FURUTA, H TERADA, H SASHIKUMA

The Role of Corrosion Pillowing in NDI and in the Structural Integrity of Fuselage Joints
J P KOMOROWSKI, N C BELINGER, R W GOULD

Analytical Predictions of the Residual Strength of Graphite Fiber-Reinforced Laminated Composites
C E HARRIS, T W COATS

An Evaluation of Damage Tolerance Characteristics of Sandwich Composite Structures
L CANDIANI, U MARIANI, M D CAPRICE, L LAZZERI

Delamination Behaviour of Spliced Fiber Metal Laminates
T J DE VRIES, A VLOT, L B J VOGELESANG, F HASHAGEN

Lessons Learned from the C17A Full Scale Airframe Durability Qualification Test Program
C BABISH, K W LIU

EH101 Airframe - The Fatigue Testing and Resulting Timely Modifications for the Production Aircraft
M L OVERD

The Duplication of Flight Loading Conditions on a Full-Scale F/A - 18 Aft Fuselage and Empennage Test Article
D GRAHAM, W MADLEY

Full Scale Structural Tests with the Same Test Airframe for Business Jet Aircraft: Feasibility Analysis
P BAYON de NOYER, D GILETTA de SAINT-JOSEPH

A Critical Review of Damage-Tolerance Methodology by Means of a Probabilistic Simulation of the Fatigue Process
A BROT

A Probabilistic Approach to Aircraft Structures Risk Assessment
G CAVALLINI, A LANCIOTTI, L LAZZERI

Experimental Investigation of Small Load Cycle Omission Levels in Helicopter Loading Spectra
R G BULLER, P E IRVING

Effects of Low-Amplitude Cycles in Spectrum Loading on a Fighter Aircraft
P V STRAZNICKY, J P WEISS, R L HEWITT

Eurofighter 2000: An Integrated Approach to Structural Health and Usage Monitoring
S R HUNT, I G HEBDEN

Making Fuselage Riveted Lap Splices with 200-Year Crack-Free Fatigue Lives
R P G MULLER, L J HART-SMITH

Fatigue Life Prediction of Riveted Lap-Splice Joints Using Small-Crack Theory
J C NEWMAN, C E HARRIS, M A JAMES, K N SHIVAKUMAR

Fatigue Crack Growth in Riveted Joints: Critical Experiments and Statistical Analyses
G SEGERFROJD, G S WANG, B PALMBERG, A F BLOM

Influence of Thickness on Crack Growth Life of Coldworked Holes
M GUILLAUME, A S KUO, V DUBOIS, B SCHMID, S MICHEL

Repair Assessment Program for Airbus A300 Aircraft
B BRANDECKER, H-J SCHMIDT

Analysis of Fatigue Crack Growth in Imperfectly Bonded Composite Patch Repairs of Cracked Aluminium Alloy Panels
S NABOULSI, S MALL, J J DENNEY

VOLUME II

POSTER PAPERS

A Comparison of 2024-T3 and 2524-T3 Aluminium Alloys Under Multi-Site Damage Scenarios
A F GRANDT Jr, D G SEXTON, P J GOLDEN, G H BRAY, R J BUCCI, M KULAK

Application and Extension of Structural Reliability Methods to Multi-Site Damage
H MILLWATER, J WU, H BURNSIDE, M MEAR

Probabilistic Assessment of the Influence of Multiple Site Cracking on the Damage Tolerance of Aircraft
I R ORISAMOLU

Effect of Periodic Tensile Overload on Fatigue Crack Behaviour in 2024-T351 Alloy in an Aggressive Environment
D SARCHAMY, M G BURNS, D LIGHT

Fatigue Crack Retardation in Aluminium Alloys by Means of Squeeze Dimpling
D SARCHAMY, S MOSS, M G BURNS, K LAWFORD, E HUNT

Influence of Residual Stresses and Plastic Deformation on the Crack Propagation of Aluminium Alloy Structures
P C GARNATZ

Fatigue and Damage Tolerance of Ageing Aircraft Structures
G I NESTERENKO

Probabilistic Damage Tolerance Analysis for Optimising In-Service Inspections
S A FORGUES, Y THERIAULT

Investigation on the Damage Tolerance Approach of Manufacturing Defects
D DUPRAT, A DAVY, L PIZZANELLI

Boundary Element Methods for Damage Tolerance Analysis of Aircraft Panels
N K SALGADO, M H ALIABADI

Comparison of Constant and Variable Amplitude Loading on FCG of Two Advanced Titanium Alloys at 25°C and 175°C
R R STEPHENS, R I STEPHENS

Fatigue Crack Closure and Fatigue Thresholds
I LE MAY

Correlation of Fracture Surface Topography with Fatigue Load History
C G SCHMIDT, T KOBAYASHI, D A SHOCKEY, T H FLOURNOY

Crack Turning Damage Tolerance Approach for Integrally Stiffened Structure
R G PETTIT, J C NEWMAN, M S DOMACK

Development and Application of an Ultrasonic NDT System for Real-Time Assessment of Fatigue Specimen Cracking
C T ROSS, N GRAY, D SARCHAMY

Durability Issues in Bonded Joint Design
L M BUTKUS, R V VALENTIN, W S JOHNSON

Analysis of Fatigue and Fretting of Three-Dimensional, Single and Double Rivet-Row Lap Joints
K IYER, P C BASTIAS, C A RUBIN, G T HAHN

Residual Stress Analysis of Cold Expanded Bushings
L REID, V MARRESE, E T EASTERBROOK

The Role of Fretting Fatigue in Aircraft Rivet Hole Cracking
C B ELLIOTT, D W HOEPPNER

Assessment of Fatigue Crack Growth from Cold Worked Holes
M PRIEST, D J SMITH, M J PAVIER

Fatigue Enhancement of Large Fastener Holes (25mm) in Thick Light Alloy (25mm) by Cold Expansion
E W O'BRIEN

Operational Loads and Usage Monitoring: The ASH-37 Solution for Flight Data Analysis
J MOHAMMADI, C OLKEIWICZ

The FAA Flight Loads Data Collection Program for Commercial Transport Aircraft
T J BARNES, T DEFIORE

Fatigue and Strength Loads Computed with Regression Equations Empirically Derived to Convert the Load Spectra to Design Values
J D YOST

Fatigue and Damage Tolerance Tests in Support of the Certification of Airbus A330/A340 Metallic Wing Structure
R A COLLINS, M S DEAN, A D WILLIAMS, M A BISHOP, B F VAN GRIENSVEN, A M ALEXANDER

Effects of Combined Loads on the Nonlinear Response of Stiffened Shells with Long Cracks
J H STARNES JR, C A ROSE, R D YOUNG, C C RANKIN

IDF Full Scale Durability Test
B D CHENG, J S CHEN, J Y HUANG

Methodology for Testing Curve Fuselage Panels under Biaxial Loading Conditions
T FLEISCHER, D SCHÖNFELD

Riveted Lap Joints of the Fiber Metal Laminate GLARE under Biaxial Loading
K H TRAUTMANN, C D DONNE, C SCHEDERA

Full Scale GLARE Fuselage Panel Tests
R W A VERCAMMEN, H H OTTENS

Delamination Suppression in Quasi-Isotropic CFRP Laminates under Fatigue Loading - Effects of Toughened Interlaminar Layers
N TAKEDA, S OGIHARA, S KOBAYASHI, A KOBAYASHI

Impacting Thin Skinned Composite Sandwich Laminates
R R AITKEN, D P W HORRIGAN, G MOLTSCHANIWSKYJ

Fatigue Damage Design Principles of Fibre-Reinforced Titanium Matrix Composites
E DE LOS RIOS, C A RODOPOULOS, J R YATES

Statistical Analysis of Fatigue Behaviour of Aluminium Alloys in the Presence of Prior Corrosion
J D BALDWIN, T B MILLS, C A PAUL

The Development of an Integrated Bonded Repair System - A Reliable Means of Giving New Life to Ageing Airframes
R FREDELL, C GUIJT, J MAZZA

Enhancements to Repair Assessment and Integrated Design (RAPID)
J G BAKUCKAS JR, J YU, R E BLAUVELT, C A BIGELOW, P W TAN

Fatigue Life Predictions for Notch Geometries in a Gas Turbine Disc Material
M R BACHE, W J EVANS, G S REES

An Assessment of the Probability of Failure Associated with the Use of a Life Factor or Two
A B MEW, A W CARDRICK

Statistics of Aircraft Accidents and Case Studies on Structure or Material Related Accidents
H TERADA