Fatigue crack growth predictions in Aramid reinforced aluminum laminates (ARALL)

Journal of Aircraft

Volumn 25, Issue 2, 1988, Pages 135-140

  Marissen, R ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS--FATIGUE; COMPOSITE MATERIALS--FIBER REINFORCED; LAMINATED PRODUCTS--FATIGUE;

ARALL; ARAMID REINFORCED ALUMINUM LAMINATES;

ALUMINUM AND ALLOYS;

EID: 0023960018     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.45553     Document Type: Article

References (16)

1. U.S. Patent Nos. 4,500,589 and 4,489,123.
2. Marissen, R. and Vogelesang, L.B., “Development of a New Hybrid Material: Aramid Reinforced Aluminium Laminate (ARALL),” Paper presented at International SAMPE Meeting, Cannes, France, Jan. 1981.
3. Vogelesang, L.B., Marissen, R., and Schijve, J., “A New Fatigue Resistant Material: Aramid Reinforced Aluminium Laminate (ARALL),” Proceedings of the 11th ICAF Symposium, Noordwijkerhout, the Netherlands, May 1981.
4. Gunnink, J.W., Vogelesang, L.B., and Schijve, J., “Application of a New Hybrid Material (ARALL) in Aircraft Structures,” Paper presented at ICAS Conference, Seattle, WA, Aug. 1982.
5. Vogelesang, L.B. and Gunnink, J.W., “ARALL, a Material for the Next Generation of Aircraft. A State of the Art,” Dept, of Aerospace Engineering, Delft University of Technology, Delft, the Netherlands, Rept. LR-400, Aug. 1983.
6. Vogelesang, L.B. and Paalvast, C.G., “The Application of Briles Rivets for Mechanical Jointing of ARALL,” Dept, of Aerospace Engineering, Delft University of Technology, Delft, the Netherlands, Rept. LR-387, June 1983.
7. Gunnink, J.W. and Rothwell, A., “An Assessment of the Static Strength of Flush Head Aluminium Alloy Rivets in Two Grades of ARALL Sheet,” Dept, of Aerospace Engineering, Delft University of Technology, Delft, the Netherlands, Rept. LR-391, July 1983.
8. Elber, W., “The Significance of Crack Closure,” ASTM STP 406, 1971, p. 330.
9. Newman, J.C. Jr., “A Finite-Element Analysis of Fatigue Crack Closure,” ASTM STP 590, 1976, p. 281.
10. Marissen, R., “Flight Simulation Behavior of Aramid Reinforced Aluminium Laminates (ARALL),” Engineering Fracture Mechanics, Vol. 19, No. 2, 1984, pp. 261-277.
11. Ratwani, M.M., “A Parametric Study of Fatigue Crack Growth Behavior in Adhesively Bonded Metallic Structures,” Transactions of the ASME, Vol. 100, Jan. 1978, pp. 46-51.
12. Rose, L.R.F., “A Cracked Plate Repaired by Bonded Reinforcements,” International Journal of Fracture, Vol. 18, No. 2, 1982.
13. Roderick, G., “Crack Propagation in Aluminium Sheets Reinforced with Boron-Epoxy,” University Microfilms, Ann Arbor, MI and University Microfilms International, London, 1978.
14. Marissen, R., “Fatigue Crack Growth in Aramid Reinforced Aluminium Laminates (ARALL): Mechanisms and Predictions,” Wissenschaftl, Berichtswesen DFVLR, Cologne, FRG, Rept. DFVLR-FB-84-37, 1984.
15. Schijve, J., van Lipzig, H.T.M., van Gestel, G.F.J.A., and Hoeymakers, A.H.W., “Fatigue Properties of Adhesive Bonded Laminated Sheet Material of Aluminium Alloys,” Dept, of Aerospace Engineering, Delft University of Technology, Delft, the Netherlands, Rept. LR-276, Dec. 1978.
16. Marissen, R., Trautmann, K.H., Foth, J., and Nowack, H., “Microcrack Growth in Aramid Reinforced Aluminium Laminates (ARALL),” Proceedings Fatigue’84 Conference, Vol. 2, Birmingham, UK, Aug. 1984, pp. 1081-1091.