The results from a theoretical and experimental investigation of the dynamic response of cylindrically curved laminated composite shells subjected to normal blast loading are presented. The dynamic equations of motion for cylindrical laminated shells are derived using the assumptions of Love's theor
β¦ LIBER β¦
Theoretical and experimental response of composite laminates with delaminations loaded in compression
β Scribed by Douglas S Cairns; Pierre J Minguet; Mohamed G Abdallah
- Publisher
- Elsevier Science
- Year
- 1994
- Tongue
- English
- Weight
- 731 KB
- Volume
- 27
- Category
- Article
- ISSN
- 0263-8223
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
STRUCTURAL RESPONSE OF LAMINATED COMPOSI
β
H.S. TΓRKMEN
π
Article
π
2002
π
Elsevier Science
π
English
β 335 KB
Delamination growth in composite laminat
β
T.L. Norman; C.T. Sun
π
Article
π
1993
π
Elsevier Science
π
English
β 734 KB
Experimental and theoretical study of st
β
J.G. Nie; C.S. Cai; H. Wu; J.S. Fan
π
Article
π
2006
π
Elsevier Science
π
English
β 772 KB
Nine specimens of steel-concrete composite beams with openings in the concrete flange were tested in the present study. The main parameters considered were the size and position of the openings. Two modes of failure were observed in the tests, depending on the loading arrangement and the position of