1 |
Baker, A. A., Dutton, S. and Kelly, D. W., 2004, "Composite Materials for Aircraft Structures," AIAA Inc., Reston, USA.
|
2 |
Cui, W. C., Wisnom, M. R. and Jones, M., 1992, "A Comparison of Failure Criteria to Predict Delamination of Unidirectional Glass/Epoxy Specimens Waisted Through the Thickness," Composites, Vol. 23, No. 3, pp. 158-166.
DOI
ScienceOn
|
3 |
Benzeggagh, M. L. and Kenane, M., 1996, "Measure of Mixed-Mode Delamination Fracture Toughness of Unidirectional Glass/Epoxy Composites with Mixed-Mode Bending Apparatus," Composites Science and Technology, Vol. 56, pp. 439-449.
DOI
ScienceOn
|
4 |
Yurko III, A. A. and Esslinger, J. R., 2005, "Affordable High Performance Composite Case Rocket Motor Manufacturing," 41st AIAA/ASME/ SAE/ASEE Joint Propulsion Conference.
|
5 |
Kim, W. S., Jang, C. J. and Lee, J. J., 2011, "Mixed-Mode Fracture Toughness Measurement of a Composite/Metal Interface," The Journal of the Korean Society for Composite Materials, Vol. 24, No. 2, pp. 1-8.
과학기술학회마을
DOI
ScienceOn
|
6 |
ASTM International, 2007, Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix Composites, ASTM D5528.
|
7 |
ASTM International, 2006, Standard Test Method for Mixed Mode I-Mode II Interlaminar Fracture Toughness of Unidirectional Fiber Reinforced Polymer Matrix Composites, ASTM D6671/D6671M.
|
8 |
James, R. R. and John. Jr, C. R., 1990, "Mixed-Mode Bending Method for Delamination Testing," AIAA Journal, Vol. 28, No. 7, pp. 1270-1276.
DOI
|
9 |
ASTM International, 2008, Standard Test Method for Strength Properties of Double Lap Shear Adhesive Joints by Tension Loading, ASTM D3528.
|
10 |
Camanho, P. P., Davila, C. G. and de Moura, M. F., 2003, "Numerical Simulation of Mixed-Mode Progressive Delamination in Composite Materials," The Journal of Composite Materials, Vol. 37, No. 16, pp. 1415-1438.
DOI
ScienceOn
|
11 |
Wang, C. H. and Chalkley, P., 2000, "Plastic Yielding of a Film Adhesive Under Multiaxial Stresses," International Journal of Adhesion & Adhesive, Vol. 20, pp. 155-164.
DOI
ScienceOn
|
12 |
Aydin, M. D., Ozel, A. and Temiz, S., 2004, "Non-linear Stress and Failure Analysis of Adhesively-Bonded Joints Subjected to a Bending Moment," International Journal of Adhesion & Adhesive, Vol. 18, No. 14, pp. 1589-1602.
|
13 |
Lee, C. J., Lee, S. K., Ko, D. C. and Kim, B. M., 2009, "Evaluation of Adhesive Properties Using Cohesive Zone Model : Mode I," Trans. Korean Soc. Mech. Eng. A, Vol. 33, No. 5, pp. 474-481.
과학기술학회마을
DOI
ScienceOn
|
14 |
Lee, Y. H., Ban, C. S., Choi, J. H. and Kweon, J. H., 2008, "Failure Load Prediction of the Composite Adhesive Joint using the Damage Zone Ratio," The Journal of the Korean Society for Composite Materials, Vol. 21, No. 4, pp. 22-28.
과학기술학회마을
|
15 |
Park, J. S., Kim, H. K., Kim, C. U., Hwang, T. K. Hong, C. S. and Kim, C. G., 2001, "Behavior Analysis and Strain Measurement of the Filament Wound Composite Tank Part I. Finite Element Analysis of the Filament Wound Tank," The Korean Society for Aeronautical & Space Sciences, Vol. 29, No. 7, pp. 49-55.
과학기술학회마을
|
16 |
Mard, F., 1993, "Design, Manufacture and Test of the Composite Case for ERINT-1 Solid Rocket Motor," 29th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
|