Study on co-cured composite panels with blade-shaped stiffeners

Composites Part A: Applied Science and Manufacturing

Volumn 34, Issue 5, 2003, Pages 403-410

  Huang, C K ^a  

^a LUNGHWA UNIVERSITY OF SCIENCE AND TECHNOLOGY   (Taiwan)

Author keywords

Blade shaped; Co cured; Composite; Film adhesive; Flange length; Radius; Secondary bonding; Stiffener; Tension force; Twisted fibers; Voids

Indexed keywords

AIRCRAFT; BONDING; COMPOSITE MATERIALS; STRENGTH OF MATERIALS; TENSILE TESTING;

TWISTED FIBERS;

STRUCTURAL PANELS;

EID: 0037544303     PISSN: 1359835X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1359-835X(03)00081-2     Document Type: Article

References (15)

1. Elaldi F., Lee S., Scott R.F. Manufacture of composite panels with J-shape stiffeners. Mater Manufact Process. 10:(1):1995;27-36.
2. Williams J.G., Stein M. Buckling behavior and structural efficiency of open-section stiffened composite compression panels. AIAA J. 14:(11):1976;1618-1626.
3. Lackman L.M., O'Brien W.L., Lloyd M.S. Edward M., Oplinger D.W., Burke J.J. Fibrous composites in structural design. 1980;125-144 Plenum Press, New York.
4. Dickson J.N., Cole R.T., Wang J.T.S. Edward M.D., Oplinger D.W., Burke J.J. Fibrous composites in structural design. 1980;313-327 Plenum Press, New York.
5. Dickson J.N., Biggers S.B., Wang J.T.S. Bunshell A.R. Advances in composite materials. 1980;812-825 Pergamon Press, Oxford.
6. Williams JG, Mikulas MM. Analytical and experimental study of structurally efficient composite hat-stiffened panels loaded in axial compression. AIAA Paper 75-754, Denver, Colo; 1975.
7. Wittrick W.H., Williams W. Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadings. Int J Mech Sci. 1974;16.
8. Verreman Y., Nie B. Early development of fatigue cracking at manual fillet welds. Fatigue Fract Engng Mater Struct. 19:(6):1996;669-681.
9. Pang H.L.J. Analysis of weld toe profiles and weld toe cracks. Int J Fatigue. 15:(1):1993;31-36.
10. Nguyen N.T., Wahab M.A. The effect of undercut, misalignment and residual stresses on the fatigue behavior of butt welded joints. Fatigue Fract Engng Mater Struct. 19:(6):1996;769-778.
11. Tsai C.L., Kim D.S. Analysis of fatigue crack propagation behavior in fillet welded T-joint. Engng Fract Mech. 36:(4):1990;653-660.
12. Huang C.K., Yang Y. Warping in advanced composite tools with varying angles and radii. Compos Part A: Appl Sci Manufact. 28A:1997;891-893.
13. Cytec Fiberite Inc. FM 300 Film Adhesive, 1300 Revolution Street, Havre De Grace, MD 21078; 1998.
14. Sikorsky material specification. SS9623 Rev. 7; 1995.
15. US Military Standard Parts. MS16998 and MS35650 Rev. E; 1976.