1 |
Michael C. Y. Niu, Composite Airframe Structure, Conmilit press LTD, Hong Kong. 1992
|
2 |
J. N. Dickson, R. T. Cole, and J. T. S. Wang, "Design of stiffened composite panels in the Post-Buckling Range," Fibrous Composites in Structural Design, Plenum Press, New York, 1980, pp. 313-327.
|
3 |
권진희, “Z-단면 복합재 스트링거의 크리플링 해석,” 한국복합재료학회지, 제12권, 제6호, 1999, pp. 65-73.
|
4 |
T. J. Stapleton, and E. A. Hoover, Fuselage Nose Internal Loads Analysis, Vol. 3, Mcdonnell Douglas, 1992, pp 3.17-3.19.
|
5 |
H. Harder. and E. Hoover, Fuselage Primary Structural Strength, Vol. 1. Mcdonnell Douglas, 1993, pp 1.8.1-1.10.29.
|
6 |
이인철, 홍창선, “보강된 복합적층 패널의 좌굴 및 좌굴후 거동,” 대한기계학회 춘계학술발표회 초록집, 1994, pp. 67-69.
|
7 |
E. F. Bruhn, Analysis and Design of Flight Vehicle Structures, S. R. Jacobs & Associates Inc., 1973
|
8 |
C. S. Hong and S. M. Jun, "Buckling Behaviar of Laminated Composite Cylindrical Panel with Initial Imperfections," Recent Developments in Buckling of Structures, ed by. D. Hui et al., PVP-Vol. 183, AD-Vol. 18, ASME, New York, 1989, PP. 9-15.
|
9 |
T. J. Allen, MD90-30 Fuselage Loads Analysis Technical Report, Mcdonnell Douglas, 1992, pp. 2.2-2.27.
|
10 |
James M. Whitney, Structural Analysis of Laminated Anisotropic Plates, Technomic Publishing AG. Pennsylvania, 1987.
|