Zobrazeno 1 - 10
of 54
pro vyhledávání: '"Waruna Seneviratne"'
Publikováno v:
International Journal of Lightweight Materials and Manufacture, Vol 3, Iss 4, Pp 426-434 (2020)
Crack root rotation is a measure of deviation from clamped boundary conditions of region in front of the crack tip. The root rotation depends on the shear force and bending moment acting at the crack tip. Such rotation significantly affects the compl
Externí odkaz:
https://doaj.org/article/59a56562cdc943098eb80fa808946c66
Publikováno v:
International Journal of Lightweight Materials and Manufacture, Vol 3, Iss 4, Pp 426-434 (2020)
Saseendran, V, Carlsson, L A, Berggreen, C & Seneviratne, W 2020, ' Crack length correction and root rotation angle in a sandwich single cantilever beam (SCB) fracture specimen ', International Journal of Lightweight Materials and Manufacture, vol. 3, no. 4, pp. 426-434 . https://doi.org/10.1016/j.ijlmm.2020.06.005
Saseendran, V, Carlsson, L A, Berggreen, C & Seneviratne, W 2020, ' Crack length correction and root rotation angle in a sandwich single cantilever beam (SCB) fracture specimen ', International Journal of Lightweight Materials and Manufacture, vol. 3, no. 4, pp. 426-434 . https://doi.org/10.1016/j.ijlmm.2020.06.005
Crack root rotation is a measure of deviation from clamped boundary conditions of region in front of the crack tip. The root rotation depends on the shear force and bending moment acting at the crack tip. Such rotation significantly affects the compl
Publikováno v:
Journal of Sandwich Structures & Materials. 23:2923-2943
Fracture testing and analysis of aerospace grade honeycomb core sandwich constructions using a single cantilever beam test methodology is presented here. Influence of various parameters such as facesheet thickness, core density, honeycomb cell-size,
Publikováno v:
American Society for Composites 2021.
The primary heat generation mechanisms of carbon fiber reinforced thermoplastic laminates during induction heating are joule losses, junction heating with contact resistance and dielectric hysteresis. In relation, these mechanisms are highly affected
Publikováno v:
American Society for Composites 2021.
Additive manufacturing has been adopted in many aerospace and defense applications to reduce weight and buy-to-fly ratios of low-volume high- complexity parts. Polymer-based additive manufacturing processes such as Fused Deposition Modeling (FDM) has
Autor:
John Tomblin, Waruna Seneviratne
Publikováno v:
AIAA Scitech 2021 Forum.
Publikováno v:
American Society for Composites 2020.
Autor:
Caleb Saathoff, Waruna Seneviratne, Xiaodong Cui, Dinh Chi Pham, Anand Vijay Karuppiah, Jim Lua
Publikováno v:
AIAA Scitech 2020 Forum.
Publikováno v:
AIAA Scitech 2020 Forum.
Autor:
Sachin Shrivastava, Jocelyn M. Seng, Sung Kyu Ha, Woo Il Lee, Pedro P. Camanho, Antonio Miravete, José Daniel Diniz Melo, Aniello Riccio, Thierry Massard, Waruna Seneviratne, Henry T. Yang, Alan T. Nettles, George S. Springer, Ajit K. Roy, H. Thomas Hahn, Yasushi Miyano, A. Arteiro, Naresh Sharma, Sangwook Sihn, Klemens Rother, Robert Rainsberger, Carlos Alberto Cimini, Tong Earn Tay, Surajit Roy, Francisco K. Arakaki, Giuseppe Catalanotti, António Marques, Pranav D. Shah, Francesco Di Caprio
Publikováno v:
Arteiro, A, Sharma, N, Melo, J D D, Ha, S K, Miravete, A, Miyano, Y, Massard, T, Shah, P D, Roy, S, Rainsberger, R, Rother, K, Cimini, C, Seng, J M, Arakaki, F K, Tay, T E, Lee, W I, Sihn, S, Springer, G S, Roy, A, Riccio, A, Di Caprio, F, Shrivastava, S, Nettles, A T, Catalanotti, G, Camanho, P P, Seneviratne, W, Marques, A T, Yang, H T & Hahn, H T 2020, ' A case for Tsai's Modulus, an invariant-based approach to stiffness ', Composite Structures, vol. 252, 112683 . https://doi.org/10.1016/j.compstruct.2020.112683
For the past six years, we have been benefiting from the discovery by Tsai and Melo (2014) that the trace of the plane stress stiffness matrix ( tr ( Q ) ) of an orthotropic composite is a fundamental and powerful scaling property of laminated compos
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::91ecc8252d99e0c81205e8ac8f58f16c
http://hdl.handle.net/11591/436728
http://hdl.handle.net/11591/436728