1 |
I. C. Taig, 'Design Concepts for the Use of Composite in Airframes', British Aircraft Co., 1975
|
2 |
R. Marrisen, 'Fatigue Mechanism in ARALL A Fatigue Resistant Hybrid Aluminium Aramid Composite Material', Fatigue, 87, Proc. 3rd Int. Cont. on Fatigue Threshold, Vol. 3, EMAS LTD, Warley, U.K, pp. 1271-1279, 1987
|
3 |
Kyung-Bong Lee, 'A study on mechanical and fatigue characteristics in a fiber reinforced metal laminates of Al/CFRP', Journal of KIIS, Vol. 14, No.5, pp. 11-15, 1999
|
4 |
J. C. McMillian, 'Bonded Joints and Preparation for Bonding', NATOAGARD Lecture Series 102, 3, #7, p. 150, 1979
|
5 |
Kyung-Bong Lee, 'The effect of CFRP volume fraction and carbon fiber orientation on tensile/flexural properties in Al/CFRP laminate', Journal of the KIIS, Vol. 16, No.5, 13-16, 2001
|
6 |
H. K. Yoon, 'The Effect of Bridging on Fatigue Crack Growth Behavior in Aramid Patched Aluminium Alloy (APAL)', J. of KSME, Vol. 8, No.4, pp. 375-384, 1994
DOI
|
7 |
D. L. Davidson, 'Fatigue Crack Growth through ARALL 4 at Ambient Temperature', Fatigue Fract. Eng. Mater. Struct., Vol. 14, No. 10, pp. 939-951, 1991
DOI
|
8 |
S. Oken, 'Analytical and experimental Investigation of Aircraft Metal Structures Reinforced with Filamentary Composites', NASA CR-1859, 1971
|
9 |
C. T. Lin, 'Fatigue Behaviour of Carbon Fiber Reinforced Aluminium Laminates', Composites, Vol. 22, pp. 135-141, 1991
DOI
ScienceOn
|
10 |
R Marrissen, 'Flight Simulation Behavior Aramid Reinforced Aluminium Laminate (ARALL)', Eng. Fracture Mechanics, 19, pp. 261-277, 1984
DOI
ScienceOn
|
11 |
D. H. Middleton, 'Composite Materials in Aircraft Structure The Involvement of the United States Aircraft Structure Industry in the Development of Advanced Composite Materials', Longman Scien tific & Technical, John Wiley Inc., New York, pp. 273-288, 1990
|
12 |
G. L. Roderick, 'Debond Propagation in Composite Reinforced Metals', NASA TMX-71948, 1974
|
13 |
F. A. Sandow, 'Composite Repair of Cracked Aluminum Alloy Aircraft Structure', AFWAL-TR-87-3072, 1987
|