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ICAF 21, 2001 - Design for Durability
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€245+€16p&pUK/€32p&pW
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Proceedings of the Twenty-first ICAF (International Committee
on Aeronautical Fatigue) Symposium, Toulouse, France, June
27-29, 2001. Editor: J. Rouchon.
ISBN 2 85428 5743 (2001), 1127 pages in 2 volumes
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Proceedings of the 21st Symposium of the International Committee
on Aeronautical Fatigue 27-29 June 2001, Toulouse, France
VOLUME I PRESENTED PAPERS
Plantema Memorial Lecture
Fatigue Science and Engineering - Achievements and Challenges ANDERS
F BLOM
The Effect of Multiple Cracking on Fatigue Crack Growth of Curved
Fuselage Panels
J G BAKUCKAS Jr, C A BIGELOW, P W TAN and L PHAM
Short Crack Growth in the Lap Joints: Experimental and Numerical
Results
G CAVALLINI, R GALATOLO, R LAZZERI
Widespread Fatigue Damage Assessment of Jet Transport Structures
M L GRUBER, B E JOHNSON and I C WHITTAKER
Structural Modifications - USAF Experience
J W LINCOLN
The Transall Life Extension Program
A SANTGERMA, C SIMON
Structural Risk Assessment of Lower Wing Skin Panels of RAAF B707
Aircraft
P JACKSON
Operational Loads Measurement of the Hawk Aircraft in RAF Service
S REED, D HOLFORD, M GELDER, S ROBERTS
Fatigue Strength and Damage Tolerance of Thin Sheet Riveted Lap/Splice
Joints with Cold-Expanded Holes
B R KRASNOWSKI, D J REDDY, B FRANADA, L REID, L J RESTIS
Knowledge-Based Automated Fatigue Analysis of Airbus Main Wingbox
Ribs
S HAN, A WILLIAMS and M R JONES
The Swiss F/A - 18 Full Scale Fatigue Test
M GUILLAUME, B BUCHER, M GIDINAT, J HAWKINS, I PFIFFNER, J WEISS,
M GOTTIER, G MANDANIS
Fatigue and Information Technology
J Y BEAUFILS, C MEYER
Effect of Load Components on Fatigue Life of Fuselage Model Structure
H TERADA, T OKADA and P A DYBSKIY TANGO
Metallic Fuselage Barrel, Validation of Advanced Technologies
H J SCHMIDT, C VOTO, J HANSSON
The Behaviour of Glare Material after a Severe Impact in a Row of
Holes or Rivet Row Containing Initial Flaws and Fatigue Damage
T DE VRIES, P HOOIJMEIJER and A VLOT
Load Enhancement Factor to be Applied on Fatigue Test for Certification
of Composites
J M RUIZ-BARRAGAN, M A MORELL FUENTES, M HUERTAS GARCIA and D FERNANDEZ
VILLALBA
Damage Tolerance of Welded Aluminium Aircraft Structures
G BUSSU, P E IRVING
Aluminium Alloy Fatigue Initiation: Existence of Two Micromechanisms
L ANQUEZ
Parametric Sensitivities Affecting the Calculated Fatigue Life of
a Fleet of Military Aircraft
S CAMPBELL
Damage Tolerance of Cold-Worked Fastener Holes
B JOURNET, E LUCIEN, F CONGOURDEAU, F VINHAS, C ITHURRALDE, D DUPRAT
Advances in Residual Strength Analyses from Laboratory Coupons to
Structural Components
J H STARNES JR, J C NEWMAN JR, C E HARRIS, R D YOUNG, C A ROSE and
M A JAMES
Impact of Corrosion on Structural Integrity
M E HOFFMAN, P C HOFFMAN, R PEREZ, K K SANKARAN, and H G SMITH JR
Statistical Characteristics of Discontinuity States and their Application
to Corrosion Risk Assessment of Aircraft Structures
M LIAO, N C BELLINGER and J P KOMOROWSKI
Nature and Distribution of Corrosion Fatigue Damage in the Wind
Skin Fastener Holes of a Boeing 707
M C LATHAM, D G HARLOW, R P WIE
Modelling of Fatigue Crack Growth from Exfoliation and Pitting Corrosion
G CLARK, P K SHARP and T MILLS
Corrosion Pitting and the Transition to Surface Fatigue Cracks in
2024-T3 Aluminium Alloy
P N CLARK and D W HOEPPNER
Assessing the Reliability of Fail-Safe Structures
A BROT
Aircraft Economic Fatigue Life Evaluation Using a Probabilistic
Approach
M OORE
Stochastic Fatigue Analysis of an F-16 Forward Engine Mount Supporting
Fitting
F P GROOTEMAN, M H OTTENS and H J TEN HOEVE
Durability Assessment of Fuselage Single Shear Lap Joint with Pads
M MILLER, G K DAS, T SOVAR
Computational Method for Evaluating the Fatigue Life of Mechanical
Joints
G S WANG
Short Crack Evolution in Countersink Geometries
D E DENMAN, J D BALDWIN, B M TAYLOR, M J FREY
VOLUME II POSTER PAPERS
Measurement of Structural Deflection on a Training Aircraft under
Manoeuvre Loading Conditions
C A MARTIN, T G GILBERT and T M LEE
Comparative Vacuum Monitoring: A New Method of In-Situ Real-Time
Crack Detection and Monitoring
D P BARTON
Evaluation of a Novel NDE Technique for Surface Crack Monitoring
Using Laboratory Fatigue Specimens
P K SHARP and G CLARK
Influence of Cold Working and Interference Fit on Fatigue Life of
7475-T7351 Aluminium Alloy Fastener Hole
S LAROUCHE, M BERNARD and T BUI-QUOC and D JULIEN
Calculation of Actuator Loads for Full-Scale Aircraft Fatigue Testing
R HISCOKS, R S RUTLEDGE, R L HEWITT
Post-Impact Biaxial Fatigue Crack Growth in Glare
J F LALIBERTÉ, C POON, P V STRAZNICKY, Z FAWAZ and K McCUAIG
Fatigue Evaluation of Thick Monolithic Aluminium Structures Repaired
Using Composite Bonded Doublers
J F ROBERGE, M B ZGELA, K W NEALE, J EIBLMEIER, N LANDRY, K McRAE
CT114 Tutor - Snowbird Aerobatic Aircraft Safety by Inspection Coupon
Test Program
M YANISHEVSKY, A DOUCHANT, M BRETON, C TURCOTTE, M SOVA
New Concept of a Local Elastic Stress Approach for Fatigue Life
Calculation
M RUZICKA, J PAPUGA
Reassessment of the Fatigue Life of Valmet Vinka Primary Trainer
Using the Actual Flight Spectrum
J PIRTOLA
Damage Tolerance Behaviour of Longitudinal Cracks in Complex Curved
Structures
C SAVES St GERMES, L ALBUGUES, A DAVY
Development and Validation of Stress Intensity Factors Under 2D
Gradient Solutions
J DESQUINES, D SORIA, A BASSOT, J L ROMERO
Biaxial Fatigue under Axial Load and Internal Pressure on TI 6-4
and Inconel 718 Alloys
V GOMEZ, D RECORBET, R CHIERAGATTI
Assessment of K-Gages Capability for K Prediction in Real Structure
Tests
P HAMEL
A Simplified Method for the Modelling of Strain Controlled LCF Test
Results Based on the Chaboche Model
F VOGEL
Fatigue Behaviour of Tapered Composite Structures - Influence of
Fibre Areal Weight and New Concepts
G MEIRINHOS, J ROCKER, J P CABANAC and J J BARRAU
Modelling the Ductile Fracture of Thin High Strength Aluminium Sheet
O CHABANET, J BESSON, J C EHRSTRÖM and W BROCKS
On Board Engine Life Usage Monitoring by Real Time Computation
M KOEHL
A340-600 Full-Scale Fatigue Test: A Further Step Forward into an
Efficient Structure Qualification
O TUSCH, K WOITHE
Fatigue Problems in the Design of Fuselage Panels in Glare
G CAVALLINI, R GALATOLO and L LAZZERI
Fatigue Problems in the Design of Fuselage Panels in Glare
G CAVALLINI, R GALATOLO and L LAZZERI
Application of a Compliance Method for Fatigue Crack Growth Analysis
of Glare 3 Fibre/Metal Laminates
T TAKAMATSU, T SHIMOKAWA, T MATSUMURA
Microscopic Damage Progress in Carbon/Bismaleimide Cross-Ply Laminate
under Fatigue Loading
S KOBAYASHI, S OGIHARA, K TERADA, N TAKEDA and A KOBAYASHI
Procedure for Estimating the Fatigue Life in Mechanically Fastened
Joints in Glare
J J HOMAN
Computer Aided Sequencing of Loads and Stresses for Fatigue Analysis
and Testing
R HOUWINK, R P G VEUL, H J TEN HOEVE
Early Detection of Cracks in 1 Stage Compressor Blades of Running
Engine
R SZCZEPANIK
Ensuring Damage Tolerance of Advanced Wide-Body Aircraft Structures
Prof. G I NESTERENKO
A New Model to Predict Corrosion Fatigue Crack Growth in Aluminium
Alloys
S A MICHEL, G SOYKA and I KONGSHAVN
Durability Prediction using Automatic Crack Growth Simulation
S MELLINGS, J BAYNHAM, R A ADEY and T CURTIN
How to Extend Fatigue Life by Understanding and Applying Surface
Engineering Principles
E R DE LOS RIOS, M ARTAMONOV, C A RODOPOULOS, P PEYRE and A LEVERS
A New Methodology for the Evaluation of Interacting Features in
Aircraft Design
R GRAHAM, L GILL, M RAINES and K SWIFT
Crack Bulging Effects in Longitudinal Cracks in Pressurised Narrow-body
Aircraft
C A BIGELOW, J G BACKUKAS Jr, P W TAN, X LEE, A RAHMAN
Life Enhancement of Structure Surrounding Load-Bearing Access Panel
Doors
L REID, J RESTIS and J RANSOM
Developing Tactical Aircraft Flight Manoeuvre Spectra: Fleet Reliability
Considerations
E S MEYER, S S FIELDS and P A REID
A Critical Comparison Between Mechanistically Based and Experientially
Based Statistical Modelling
D G HARLOW, R P WEI
Fatigue Life Prediction in Aluminium Alloys without the use of ?Kth
E A DEBARTOLO and B M HILLBERRY
A Critical Point-In-The-Sky Approach to Master Event Spectrum Development
T N CALLIHAN
Fatigue Behaviour of 7075 T6 Aluminium Alloy in Aggressive Environments
V AGARWALA, B SHAFIQ
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