Aeronautical Fatigue Publications and Books:

ICAF 21, 2001 - Design for Durability

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