Damage tolerance implications of corrosion pillowing on fuselage lap joints

Journal of Aircraft

Volumn 35, Issue 3, 1998, Pages 487-491

  Bellinger, N C ^a   Komorowski, J P ^a   Gould, R W ^a  

^a NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

CORROSION; CRACK PROPAGATION; FINITE ELEMENT METHOD; STRESS ANALYSIS; STRESS INTENSITY FACTORS;

CORROSION PILLOWING; FUSELAGE LAP JOINTS;

FUSELAGES;

EID: 0032069658     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2322     Document Type: Article

References (8)

1. Bellinger, N. C., Krishnakumar, S., and Komorowski, J. P., "Modelling of Pillowing Due to Corrosion in Fuselage Lap Joints," CAS Journal, Vol. 40, No. 3, 1994, pp. 125-130.
2. Bellinger, N. C., and Komorowski, J. P., "Corrosion Pillowing Stresses in Fuselage Lap Joints," AIAA Journal, Vol. 35, No. 2, 1997, pp. 317-320.
3. Bellinger, N. C., and Komorowski, J. P., "Implications of Corrosion Pillowing on the Structural Integrity of Fuselage Lap Joints," Proceedings of the FAA-NASA Symposium on Continued Airworthiness of Aircraft Structures (Atlanta, GA), Vol. 2, DOT/FAA/AR-97/ 2, II, 1996, pp. 391-402.
4. Gruber, M. L., Mazar, C. J., Wilkins, K. E., and Worden, R. E., "Investigation of Fuselage Structure Subject to Widespread Fatigue Damage," DOT/FAA/AR-95/47, Final Rept., Feb. 1996.
5. Komorowski, J. P., Bellinger, N. C., Gould, R. W., Marincak, A., and Reynolds, R., "Quantification of Corrosion in Aircraft Structures with Double Pass Retroreflection," Canadian Aeronautics and Space Journal, Vol. 42, No. 2, 1996, pp. 76-82.
6. Bueno, C., Barker, M. D., Barry, R. C., and Betz, R. A., "Corrosion Detection and Characterization Using High Resolution Real-Time Radiography," SAMPE 41st International Symposium and Exhibition, March 1996.
7. Komorowski, J. P., and Gould, R. W., "DAIS-250C Field Inspections at First Air," LTR-ST-2073, Sept. 1996.
8. Swift, T., "Widespread Fatigue Damage Monitoring - Issues and Concerns," FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance (Hampton, VA), Pt. 2, NASA-CP-3274-PT-2, 1994, pp. 829-870.