Reliable Stress and Fracture Mechanics Analysis of Complex Aircraft Components (Englisch)
- Neue Suche nach: Andersson, B.
- Neue Suche nach: Falk, U.
- Neue Suche nach: International Committee on Aeronautical Fatigue
- Neue Suche nach: Andersson, B.
- Neue Suche nach: Falk, U.
- Neue Suche nach: Blom, A. F.
- Neue Suche nach: International Committee on Aeronautical Fatigue
In:
Durability and structural integrity of airframes
;
389-412
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1993
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ISBN:
- Aufsatz (Konferenz) / Print
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Titel:Reliable Stress and Fracture Mechanics Analysis of Complex Aircraft Components
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Beteiligte:Andersson, B. ( Autor:in ) / Falk, U. ( Autor:in ) / Blom, A. F. / International Committee on Aeronautical Fatigue
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Kongress:17th Symposium, Durability and structural integrity of airframes ; 1993 ; Stockholm
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Erschienen in:
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Verlag:
- Neue Suche nach: EMAS
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Erscheinungsdatum:01.01.1993
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Format / Umfang:24 pages
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Anmerkungen:In 2 vols; Also known as ICAF '93
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ISBN:
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Medientyp:Aufsatz (Konferenz)
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Format:Print
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Sprache:Englisch
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Schlagwörter:
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Datenquelle:
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Inhaltsverzeichnis Konferenzband
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 3
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14th Plantema Memorial Lecture: Damage Tolerance - Facts and Fiction -Goranson, U. G. / International Committee on Aeronautical Fatigue et al. | 1993
- 107
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An Empirical Design Model for Fatigue Damage on the Basis of Acoustic Emission MeasurementsBerkovits, A. / Fang, D. / International Committee on Aeronautical Fatigue et al. | 1993
- 127
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Limits of Representative Acoustic Fatigue PredictionKoenig, K. / International Committee on Aeronautical Fatigue et al. | 1993
- 146
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Validation of Life Prediction Models from Representative Testings on Aluminium Alloy SpecimensBleuzen, C. / Chaudonneret, M. / Flavenot, J. / Ranganathan, N. / International Committee on Aeronautical Fatigue et al. | 1993
- 175
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Calculation Method for Predicting the Fatigue Life of Riveted JointsHoman, J. J. / Jongebreur, A. A. / International Committee on Aeronautical Fatigue et al. | 1993
- 191
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Fretting Fatigue in Aircraft JointsHoeppner, D. W. / Adibnazari, S. / International Committee on Aeronautical Fatigue et al. | 1993
- 207
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Residual Stress Distributions around Cold Expanded HolesOzdemir, A. T. / Cook, R. / Edwards, L. / International Committee on Aeronautical Fatigue et al. | 1993
- 239
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Dynamic Crack Curving at the Tear Strap with MSDShimamoto, A. / Kosai, M. / Kobayashi, A. S. / Tan, P. / International Committee on Aeronautical Fatigue et al. | 1993
- 259
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Practical Evaluation of Crack Detection Capability for Visual Inspection in JapanEndoh, S. / Tomita, H. / Asada, H. / Sotozaki, T. / International Committee on Aeronautical Fatigue et al. | 1993
- 281
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Influence of Initial Defect Conditions on Structural Fatigue in RAAF AircraftBarter, S. A. / Clark, G. / Goldsmith, N. T. / International Committee on Aeronautical Fatigue et al. | 1993
- 305
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Predicting the Influence of Initial Material Quality on Fatigue LifeHinkle, A. J. / Grandt, A. F. / International Committee on Aeronautical Fatigue et al. | 1993
- 321
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Probabilistic Durability Analysis Methodology for Metallic AirframesManning, S. D. / Yang, J. N. / International Committee on Aeronautical Fatigue et al. | 1993
- 347
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A Mechanistically Based Probability Approach for Predicting Corrosion and Corrosion Fatigue LifeWei, R. P. / Harlow, D. G. / International Committee on Aeronautical Fatigue et al. | 1993
- 367
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CF116 Upper Wing Skin Compression Induced Fatigue Cracking: A Case StudyRaizenne, M. D. / Simpson, D. L. / Zgela, M. B. / Bateman, G. / International Committee on Aeronautical Fatigue et al. | 1993
- 389
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Reliable Stress and Fracture Mechanics Analysis of Complex Aircraft ComponentsAndersson, B. / Falk, U. / International Committee on Aeronautical Fatigue et al. | 1993
- 413
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Residual Strength of Fuselage Panels with Wide Spread Fatigue DamagePark, J. H. / Singh, R. / Pyo, C. R. / Atluri, S. N. / International Committee on Aeronautical Fatigue et al. | 1993
- 443
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A Fracture Criterion for Widespread Cracking in Thin-Sheet Aluminium AlloysNewman, J. C. / Dawicke, D. S. / Sutton, M. A. / Bigelow, C. A. / International Committee on Aeronautical Fatigue et al. | 1993
- 469
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An Analytical Approach to Multi - Site DamageNathan, A. / Brot, A. / International Committee on Aeronautical Fatigue et al. | 1993
- 493
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Damage Tolerance of Fuselage Panels with Widespread Fatigue DamageTong, P. / Greif, R. / Chen, L. / Jeong, D. Y. / International Committee on Aeronautical Fatigue et al. | 1993
- 521
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Optimum Aircraft Structural Design and Verification for UsersKobayashi, S. / International Committee on Aeronautical Fatigue et al. | 1993
- 557
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The Evolution of the BAe Hawk and its Structural ClearanceO'Hara, J. / International Committee on Aeronautical Fatigue et al. | 1993
- 577
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Full Scale Structural Testing as a Tool in Managing Aging AircraftBrown, K. E. / International Committee on Aeronautical Fatigue et al. | 1993
- 589
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Aerospatiale Probabilistic Methods Applied to Aircraft MaintenanceTisseyre, M. / Plantec, J. Y. / Beaufils, J. Y. / Boetsch, R. / International Committee on Aeronautical Fatigue et al. | 1993
- 619
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Design Parameters and Variability in the Aircraft Sizing Process - Aspects of Damage ToleranceAnsell, H. / Johansson, T. / International Committee on Aeronautical Fatigue et al. | 1993
- 641
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Assessment of Structural Reliability Derived from Durability TestingLincoln, J. W. / International Committee on Aeronautical Fatigue et al. | 1993
- 659
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Application of Full Scale Test Results to Structural ModificationGottier, M. / Kuo, A. / McCord, S. / International Committee on Aeronautical Fatigue et al. | 1993
- 679
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Results of Fatigue and Damage Tolerance Test on Fokker 50 Forward FuselageFraterman, N. J. / Kummel, P. H. / International Committee on Aeronautical Fatigue et al. | 1993
- 711
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Correlation of T-37B Damage Tolerance Analyses with Full-Scale and Coupon Fatigue Test ResultsCardinal, J. W. / Wieland, D. H. / International Committee on Aeronautical Fatigue et al. | 1993
- 733
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Correlation Between Material Properties and Damage Tolerance Behaviour of Composite StructuresGerharz, J. J. / Schopfel, A. / Huth, H. / International Committee on Aeronautical Fatigue et al. | 1993
- 759
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Fatigue Test for CFRP Horizontal StabilizerTakaki, J. / Kimura, J. / Berner, J. K. / Hirahara, M. / International Committee on Aeronautical Fatigue et al. | 1993
- 775
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Fatigue Behaviour of a Glass Fibre/Epoxy Glider WingLoh, A. / Mileshkin, N. / Patching, C. A. / Wood, L. A. / International Committee on Aeronautical Fatigue et al. | 1993
- 793
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CF116 (CF-5) Full Scale Durability and Damage Tolerance Test (FSDATT)Beauvais, Y. / International Committee on Aeronautical Fatigue et al. | 1993
- 811
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CF-18 Fighter FS 488 Bulkhead Post-ECP 45/320 Flight Strain SurveyLamanque, D. / Barrett, N. / International Committee on Aeronautical Fatigue et al. | 1993
- 839
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A Study on Engineering Small Crack Growth under both Elastic and Elasto-Plastic ConditionsMingzhong, Z. / Zhongyi, Q. / International Committee on Aeronautical Fatigue et al. | 1993
- 855
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Microstructural Sensitive Fatigue Crack Growth in Al-Li 8090Xin, X. J. / De los Rios, E. R. / Navarro, A. / International Committee on Aeronautical Fatigue et al. | 1993
- 883
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The Effect of the Grinding Condition on Short Fatigue Crack Growth in Waspaloy at 19CBaobaid, J. S. / Yates, J. R. / International Committee on Aeronautical Fatigue et al. | 1993
- 899
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Fretting-Fatigue Behaviour of Major Helicopter Alloys and Influence of Surface ProtectionsFoulquier, J. / Petiot / International Committee on Aeronautical Fatigue et al. | 1993
- 917
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Ground Dynamic Response of the AircraftMartin-Siefried, Y. / Cahierre, F. / International Committee on Aeronautical Fatigue et al. | 1993
- 941
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Fatigue Life and Bird Strike Resistance of a Composite Fan Blade for Advanced Ducted EnginesFrischbier, J. / Sikorski, S. / Peter, O. / International Committee on Aeronautical Fatigue et al. | 1993
- 957
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Delamination of Fiber-Reinforced Plastics under Cyclic Mode II Loading: Crack Growth Laws and their Statistical EvaluationKussmaul, K. / Von Alberti, M. / Eisele, U. / Schneider, T. / International Committee on Aeronautical Fatigue et al. | 1993
- 971
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Local Stiffening of Shell Structures by SKO and CAO - A Method to find Fatigue Resistant and Light-Weight in EngineeringWalther, F. / Mattheck, C. / International Committee on Aeronautical Fatigue et al. | 1993
- 981
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Mean Stress Models for Low Cycle Fatigue of a Nickel-Base Super AlloyFang, D. / Berkovits, A. / International Committee on Aeronautical Fatigue et al. | 1993
- 1009
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Fatigue and Damage Mechanics of Notched, Impacted and Jointed Thermoplastic CompositesGiavotto, V. / Caprile, C. / Sala, G. / International Committee on Aeronautical Fatigue et al. | 1993
- 1029
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Fatigue Behaviour of Electron Beam Welded Joints for Helicopter TransmissionsDonzelli, G. / Paracchini, F. / Filipas, P. / International Committee on Aeronautical Fatigue et al. | 1993
- 1041
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Effect of Stress Ratio on Durability of Fiber-Reinforced CompositesAndersons, J. / Limonov, V. A. / Mikelsons, M. / International Committee on Aeronautical Fatigue et al. | 1993
- 1053
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Description of the CN-235 Fatigue Load Monitoring ProgrammeLameris, J. / Dominicus, J. / Kamil, S. / Suryo, D. / International Committee on Aeronautical Fatigue et al. | 1993
- 1069
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The Fokker Barrel Test ProgramDe Haan, P. H. / Hamelink, J. / Hoogervorst, W. P. / Pronker, W. F. / International Committee on Aeronautical Fatigue et al. | 1993
- 1085
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Aircraft Fatigue and Crack Growth Considering Loads by Structural ComponentYost, J. D. / International Committee on Aeronautical Fatigue et al. | 1993
- 1099
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Corrosion Fatigue Crack Growth Rates in Aluminium Alloys subjected to Variable Ripple SequencesPaulson, A. D. / Hoeppner, D. W. / International Committee on Aeronautical Fatigue et al. | 1993
- 1117
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Neural Network Processing of Low Frequency Eddy Current Signals for Crack DetectionHazen, D. J. / International Committee on Aeronautical Fatigue et al. | 1993
- 1121
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Split Sleeve Cold Expansion as a Rework Process for Previously Cold Expanded HolesReid, L. / International Committee on Aeronautical Fatigue et al. | 1993
- 1141
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Evaluation of Current Analytical Methods for Crack Growth in a BoltLiu, A. F. / International Committee on Aeronautical Fatigue et al. | 1993
- 1157
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Thermographic NDE Application for Quantitative Disbond and Corrosion Detection in Aircraft SkinSyed, H. I. / Winfree, W. P. / Cramer, K. E. / International Committee on Aeronautical Fatigue et al. | 1993
- 1167
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Influence of Ageing Aircraft Programs on the MD-II Damage Tolerance Certification ProcessLudas, K. J. / International Committee on Aeronautical Fatigue et al. | 1993
- 1191
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Stress - Intensity Factor Solutions for Cracks at Countersunk Rivet Holes under Uniaxial TensionTan, P. W. / Bigelow, C. A. / O'Donoghue, P. E. / Atluri, S. N. / International Committee on Aeronautical Fatigue et al. | 1993