ICAF 2009, Bridging the Gap between Theory and Operational Practice: Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Netherlands, 27-29 May 2009

Voorkant
M. Bos
Springer Science & Business Media, 24 mei 2009 - 1370 pagina's
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The 31st Conference and the 25th Symposium of the International Committee on Aeronautical Fatigue will be hosted in Rotterdam, The Netherlands, by the National Aerospace Laboratory NLR, under the auspices of the Netherlands Association of Aeronautical Engineers NVvL, the Technical University of Delft and Stork Fokker AESP B.V.

These Proceedings will consist of reviews of aeronautical fatigue activities presented by the national delegates of the 14 member nations of ICAF. It will also contain specialist papers presented by international authors with design, manufacturing, airworthiness regulations, operations and research backgrounds. The papers will be based on the theme “Bridging the gap between theory and operational practice”.

 

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Inhoudsopgave

A TEST CONCEPT FOR FUTURE AIRCRAFT FUSELAGE PANELS
3
MARKER LOADS FOR QUANTITATIVE FRACTOGRAPHY OF FATIGUE CRACKS IN AEROSPACE ALLOYS
15
SUBSTANTIATIONS OF AN AIRBORNE COMPOSITE RADOME MOUNTED ON AN AIRCRAFT DOME
55
DEVELOPMENT OF A LOW STRESS CRITERION THAT ELIMINATE A LARGE PORTION OF THE AIRCRAFT FROM DAMAGE TOLERANC...
60
DAMAGE TOLERANCE PHILOSOPHY FOR BONDED AIRCRAFT STRUCTURES
73
Damage tolerance for the structural honeymoon
91
SURVEY OF STRUCTURAL REPAIRS AND ALTERATIONS IN TRANSPORT CATEGORY AIRPLANES
108
ENHANCED TEARDOWN OF EXSERVICE FA 18ABCD CENTRE FUSELAGES
123
A CASE STUDY OF MULTIPLESITE FATIGUE CRACK GROWTH IN THE F18 HORNET BULKHEAD
707
EXPERIMENTAL AND THEORETICAL COMPARISON OF SOME MULTIAXIAL FATIGUE DESIGN CRITERIA IN THE CONTEXT OF LIFE ...
743
A CONTRIBUTION OF ENVIRONMENTAL INVESTIGATIONS FOR GLARE RIVETED JOINT SIZING
765
ADVANCES IN CRACK GROWTH MODELLING OF 3D AIRCRAFT STRUCTURES
789
DEVELOPMENT OF ADVANCED RISK ASSESSMENT METHODOLOGIES FOR AIRCRAFT STRUCTURES CONTAINING MSDMED
810
CRACK GROWTH IN FIBRE METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING
839
EFFECT OF RESIDUAL STRESSES FROM SHOT PEENING ON FATIGUE STRENGTH AND THRESHOLD TO CRACK PROPAGATION OF AL ...
859
EXPERIMENTAL VALIDATION OF STRESS INTENSITY FACTOR SOLUTIONS FOR THE PIN LOADED LUG
871

GLARE TEARDOWNS FROM THE MEGALINER BARREL MLB FATIGUE TEST
144
30 YEARS OF DAMAGE TOLERANCE HAVE WE GOT IT RIGHT?
169
COMPILATION OF DAMAGE FINDINGS FROM MULTIPLE RECENT TEARDOWN ANALYSIS PROGRAMS
187
DETECTION OF ARRESTED CRACK FOR FOAM CORE SANDWICH STRUCTURES USING OPTICAL FIBER SENSORS EMBEDDED IN A CR...
208
CONCEPT OF THE NEW A320 FATIGUE TEST
223
THE USE OF COMPOSITE MATERIAL STRIPS TO EXTEND THE DAMAGETOLERANCE LIFE OF INTEGRALLY STIFFENED ALUMINUM ...
237
STRUCTURAL INTEGRITY OF A WING UPPER SKIN WITH EXFOLIATION CORROSION
245
HELICOPTER STRUCTURAL INTEGRITY PROGRAM OF POLISH Mi24 HIND HELICOPTERS
263
OVERVIEW OF DSTO DEVELOPMENTS
278
EVALUATION MODIFICATION AND DAMAGE TOLERANCE OF AN IN SERVICE AIRCRAFT CRITICAL AREA
301
DEVELOPMENT OF A BEST PRACTICES HANDBOOK
328
FATIGUE LIFETIME IMPROVEMENT OF ARRESTMENT HOOK SHANKS BY APPLICATION OF LASER PEENING
355
DESIGN AND TESTING OF ADVANCED COMPOSITE LOAD INTRODUCTION STRUCTURE FOR AIRCRAFT HIGH LIFT DEVICES
365
HYBRID STRUCTURE SOLUTION FOR THE A400M WING ATTACHMENT FRAMES
375
CONTROL OF CRACK GROWTH RATES AND CRACK TRAJECTORIES FOR ENHANCED FAIL SAFETY AND DAMAGE TOLERANCE IN W...
386
DURABILITY AND DAMAGE TOLERANCE OF BONDED REPAIRS TO METALLIC FUSELAGE STRUCTURE
407
INVESTIGATION ON THE DESIGN OF BONDED STRUCTURES FOR INCREASED DAMAGE TOLERANCE
426
AN EXPERIMENTAL INVESTIGATION ON THE FATIGUE PERFORMANCE OF RIVETED LAP JOINTS
449
IMPROVING THE FATIGUE LIFE OF AERONAUTICAL SINGLELAP BOLTED JOINTS THANKS TO THE HYBRID BOLTEDBONDED JOINI...
474
AN EXPERIMENTAL APPROACH TO INVESTIGATE DETAILED FAILURE MECHANISMS IN FIBRE METAL LAMINATES
493
EXPERIMENTAL DETERMINATION OF ENERGY RELEASE RATE OF CFRP STRUCTURES BY MEANS OF TRANSVERSE CRACK TENSIO...
513
TOWARDS AIRCRAFT WING STRUCTURE INSENSITIVE TO FATIGUE
529
PRACTICAL APPLICATIONS OF IMPROVEMENTS IN FML CRACK BRIDGING THEORY
539
SIMULATION OF THE STRESS DISTRIBUTION ON FUSELAGE STRUCTURES FOR THE PRE AND POST ANALYSES OF CURVED PANEL T...
559
LOW CYCLE LIFETIME PREDICTION OF AL2024 ALLOY
568
FATIGUE AND DAMAGE TOLERANCE ASPECTS OF METAL LAMINATES
585
THREE DECADES OF BRIDGING THE GAP BETWEEN THEORY AND OPERATIONAL PRACTICE
600
DETAILED STRAIN FIELD ANALYSES OF FATIGUE CRACKS IN FRICTION STIR WELDED JOINTS
617
A STUDY OF INTERACTION AND COALESCENCE OF MICRO SURFACE FATIGUE CRACKS IN ALUMINIUM 7050
643
FRACTURE BEHAVIOUR OF SKIN MATERIALS OF CIVIL AIRPLANE STRUCTURES
661
FATIGUE LIFE PREDICTION OF SMALL NOTCHED TI6AL4V BASED ON THE THEORY OF CRITICAL DISTANCE
684
PROPERTIES OF FATIGUE CRACK PROPAGATION IN FRICTION STIR WELDED 2024T3 ALUMINUM ALLOY
899
FATIGUE CRACK GROWTH IN THICK PLATE 7050 ALUMINUM
909
FATIGUE LIFE EVALUATION ON TENSION TYPE FITTING
921
ACCELERATED FATIGUE TESTING ON HYDRAULIC SHAKER
931
METHODS FOR FEM ANALYSIS OF RIVETED JOINTS OF THINWALLED AIRCRAFT STRUCTURES WITHIN THE IMPERJA PROJECT
939
ON THE CRACK GROWTH BEHAVIOR UNDER SIMPLE COMPRESSIVE LOADS OF 2024T3 ALUMINIUM ALLOY
968
AN ANALYTICAL MODEL FOR LOAD TRANSFER IN A MECHANICALLY FASTENED DOUBLELAP JOINT
987
SIMULATION OF FATIGUE CRACK GROWTH IN THE HIGH SPEED MACHINED PANEL UNDER THE CONSTANT AMPLITUDE AND SPE...
1005
DISBOND PROPAGATION TESTING AND MODELLING
1019
THREE DIMINSIONAL CRACK GROWTH PREDICTION
1035
INITIAL EXPERIMENTS
1069
PILATUS PC21 A DAMAGE TOLERANT AIRCRAFT
1085
INTRODUCTION TO SERVICE OF AN ARTIFICIAL NEURAL NETWORK BASED FATIGUE MONITORING SYSTEM
1093
TOWARDS AUTOMATED FLIGHT MANEUVERSPECIFIC FATIGUE ANALYSIS
1120
SERVICE HISTORY ANALYSIS AND TEARDOWN EVIDENCE KEY ELEMENTS FOR STRUCTURAL USAGE MONITORING OF AN AGEIN...
1135
DEVELOPMENT OF FATIGUE LIFE MONITORING OF RMAF FIGHTER AIRPLANES
1155
RESEARCH AND DEVELOPMENT OF IMPACT DAMAGE DETECTION SYSTEM FOR AIRFRAME STRUCTURES USING OPTICAL FIBER SE...
1165
FIRST COMPARISONS BETWEEN DESIGN AND INFLIGHT RECORDED DATA ON EUROFIGHTER TYPHOON ITALIAN FLEET
1177
STRUCTURES
1187
A HANDSON APPROACH
1198
F35 JOINT STRIKE FIGHTER STRUCTURAL PROGNOSIS AND HEALTH MANAGEMENT AN OVERVIEW
1215
AN OVERALL BENEFIT TO COMMERCIAL AVIATION
1217
FATIGUE DAMAGE TOLERANCE OF HYBRID MATERIALS STRUCTURES SOME MYTHS FACTS FAIRYTALES
1245
INCONEL 718
1261
THE VARIABLE EXPANSION PROCESS A NEW COST EFFICIENT METHOD FOR COLD WORKING FASTENER HOLES IN ALUMINIUM A...
1275
STRESS MEASUREMENTS WITH XRAY DIFFRACTOMETRY ON ALUMINUM ALLOYS DETERMINATION OF THE MOST OPTIMIZED PA...
1285
DELAMINATION GROWTH AT INTERFACES IN HYBRID MATERIALS AND STRUCTURES UNDER VARIOUS OPENING MODES
1305
DEVELOPMENTS IN METAL BONDING
1320
ON SEPARATING THE EFFECT OF CORROSION ON INTERLAMELLAR FATIGUE OF THIN SHEET AA7079T6
1343
AUTHORS INDEX
1365
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