European FITNET Fitness-for-Service Procedure ... - Congrex

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Un-stiffened base metal panel Base material Al 6013 T6 Base material Al 6013 T6 FITNET Option 3 • Very good agreement with experiment • Used as validation of the FITNET FFS Procedure Test FITNET Option 3 FITNET Option 1 Yield Load E. Seib, PhD Thesis, 2005 ESA/ESTEC Workshop on Fracture Control, Noordwijk, NL, 9-10 Feb. 2009 M. Kocak, V. Uz, GKSS 22
Un-stiffened LBW and FSW panels LBW FSW a 0 • CTOD δ 5 R-curve obtained from C(T)50 5 R-curve obtained from C(T)50 • m = 2.0 yields best prediction ESA/ESTEC Workshop on Fracture Control, Noordwijk, NL, 9-10 Feb. 2009 M. Kocak, V. Uz, GKSS 23 δ 5 = 2 KI mER p 0.2W a 0 ⋅ [ f (Lr) ] −2 E. Seib, PhD Thesis, 2005
Page 1 and 2: Workshop on Fracture Control of Spa
Page 3 and 4: Metallic Airframe: Fabrication Tech
Page 5 and 6: Source: AIRBUS Laser Beam Welding o
Page 7 and 8: Testing and Analysis Steps FULL SCA
Page 9 and 10: • 39 Member organisations* from 1
Page 11 and 12: Fitness for Service Fracture Creep
Page 13 and 14: FITNET FFS: Section 9 Corrosion •
Page 15 and 16: Comparison of finite element and FI
Page 17 and 18: Crack After H-J. Schmidt, AeroStruc
Page 19 and 20: LBW clip-to-skin T-joint LB Welded
Page 21: Principle of residual strength pred
Page 25 and 26: Large Panel Testing Programme at th
Page 27 and 28: K-factor in stiffened panels String
Page 29 and 30: Residual Strength Prediction „sim
Page 31 and 32: Residual Strength Prediction • FI
Page 33 and 34: Residual Strength Prediction Residu
Page 35 and 36: www.eurofitnet.org FITNET FFS Proce
Page 37 and 38: Transferability of R-curves Base ma

European FITNET Fitness-for-Service Procedure ... - Congrex

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