Glare Patching Efficiency Studies

Advances in the Bonded Composite Repair of Metallic Aircraft Structure

Volumn 1-2, Issue , 2002, Pages 399-414

  Fredell, R ^a   Guijt, C ^a  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MANUFACTURE; AIRFRAMES; BORON; FUSELAGES; HYBRID MATERIALS;

AIRCRAFT STRUCTURE; CURING TEMPERATURE; EFFICIENCY STUDIES; FUSELAGE STRUCTURES; LOW TEMPERATURES; MISMATCH PROBLEMS; SERVICE TEMPERATURE; THERMAL COMPATIBILITY;

GLARE;

EID: 84940833924     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1016/B978-008042699-0/50016-4     Document Type: Chapter

References (19)

1. Baker A.A., Jones R. Bonded Repair of Aircraft Structures 1988, Martinus Nijhoff Publishers, Boston. A.A. Baker, R. Jones (Eds.).
2. Fredell R., Gunnink J. Fiber metal laminates for improved structural integrity. Proc. of the Int. Workshop on Structural Integrity of Ageing Aircraft 1992, 362-375.
3. Fredell R., Vlot A., Roebroeks R. Fiber metal laminates: New frontiers in damage tolerance. Proc. of the 15th Int. European Conference of the Society for the Advancement of Material and Process Engineering 1994, 319-328.
4. Fredell R. Damage Tolerant Repair Techniques for Pressurized Aircraft Fuselages 1994, WL-TR-94-3134, Wright-Patterson Air Force Base Ohio, June.
5. Fredell R., van Barneveld W., Vlot A. Analysis of composite crack patching of fuselage structures: High patch elastic modulus isn't the whole story. Proc. of the 39th Int. SAMPE Symposium and Exhibition 1994, 610-623.
6. Rose L.R.F. An application of the inclusion analogy. Int. J. Solids and Structures 1981, 17:827-838.
7. Rose L.R.F. Theoretical Analysis of Crack Patching. Bonded Repair of Aircraft Structures 1988, 77-106. Kluwer Academic Publishers, Dordrecht. Baker, Jones (Eds.).
8. Muki, R. and Sternberg, E. Int. J. Solids and Structures, 4, pp. 75-94.
9. Tarn J.Q., Shek K.L. Analysis of cracked plates with a bonded patch. Engineering Fracture Mechanics 1991, 40(6):1055-1065.
10. Chu R.C., Ko T.C. Isoparametric shear spring element applied to crack patching and instability. Theoretical and Applied Fracture Mechanics 1989, 11:93-102.
11. Jones R., Callinan R.J. J. Structural Mechanics 1980, 8(2):143-149.
12. Marissen, R. Fatigue Crack Growth in ARALL. Ph.D. thesis, Department of Aerospace Engineering, Delft University of Technology, Delft, the Netherlands,.
13. Roebroeks G.H.J.J. Towards GLARE: The Development of a Fatigue Insensitive and Damage Tolerant Material. Ph.D. thesis, Department of Aerospace Engineering, Delft University of Technology, Delft, the Netherlands 1991, December.
14. Rose L.R.F. Residual Thermal Stresses. Bonded Repair of Aircraft Structures 1988, 90-91. Kluwer Academic Publishers, Dordrecht. Baker, Jones (Eds.).
15. Baker A.A., Davis M.J., Hawkes G.A. Proc. 10th Int. Symp. of the Int. Comm. on Aeronautical Fatigue 1979, paper 4.3.
16. Rose L.R.F. Int. J. Fracture 1982, 18:135-144.
17. Baker A.A. Crack Patching: Experimental Studies, Practical Applications, from Bonded Repair of Aircraft Structures 1988, 107-172. Kluwer Academic Publishers, Dordrecht. Baker, Jones (Eds.).
18. Verhoeven S. Service Effects on Crack Growth Under Bonded Composite Repairs. Masters thesis, Department of Aerospace Engineering, Delft University of Technology Delft, the Netherlands 1988, July.
19. Guijt C., Fredell R. Delamination Effects in Fuselage Crack Patching 1996, SAMPE Anaheim.