Zobrazeno 1 - 10
of 13
pro vyhledávání: '"VIJAY K. GOYAL"'
Autor:
VIJAY K. GOYAL, AUSTIN PENNINGTON
Publikováno v:
American Society for Composites 2022.
The aerospace industry uses composite multi-hat stiffened panels for skins because of their high strength-to-weight and stiffness-to-weight ratios. However, laminated composites with initial flaws are susceptible to delamination under buckling loads.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9f42a33f29907eabeaaf0f9fdcec8c26
https://doi.org/10.12783/asc37/36425
https://doi.org/10.12783/asc37/36425
Publikováno v:
American Society for Composites 2021.
The high strength-to-weight and stiffness-to-weight ratio materials, such as laminated composites, are advantageous for modern aircraft. Laminated composites with initial flaws are susceptible to delamination under buckling loads. PDA tools help enha
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::08c96b3a715c8cfd3886fcf293759cab
https://doi.org/10.12783/asc36/35773
https://doi.org/10.12783/asc36/35773
Autor:
Rakesh K. Kapania, Vijay K. Goyal
Publikováno v:
Thin-Walled Structures. 46:1359-1369
A stability analysis of laminated beam structures subject to subtangential loading, a combination of conservative and nonconservative tangential follower loads, using the dynamic criterion is performed. These loads are characterized using a nonconser
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::efbc642bbd9f11d5f7ee183ed840b3b3
https://doi.org/10.1016/j.tws.2008.03.014
https://doi.org/10.1016/j.tws.2008.03.014
Autor:
Vijay K. Goyal, Rakesh K. Kapania
Publikováno v:
International Journal of Solids and Structures. 45(10):2799-2817
Because of the inherent complexity of fiber-reinforced laminated composites, it can be challenging to manufacture composite structures according to their exact design specifications, resulting in unwanted material and geometric uncertainties. Thus th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a5509cf1b41be98c732bfc4264aaaf1e
Publikováno v:
Composite Structures. 82:434-446
A new strength-fracture model is proposed for the formulation of decohesion elements, which are implemented in finite element models to predict failure of bonded joints. The proposed model unifies criteria for strength to predict failure initiation a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84233bdb3bf3c5cb021c3ba657a73505
https://doi.org/10.1016/j.compstruct.2007.01.029
https://doi.org/10.1016/j.compstruct.2007.01.029
Autor:
Vijay K. Goyal, Rakesh K. Kapania
Publikováno v:
Finite Elements in Analysis and Design. 43:463-477
A 21 degree-of-freedom element, based on the FSDT, is derived to study the response of unsymmetrically laminated composite structures subject to both static and dynamic problems. In the FSDT model used here we have employed an accurate model to obtai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8cbf669faf6316c09ccf8ffec90e9a8e
https://doi.org/10.1016/j.finel.2006.11.011
https://doi.org/10.1016/j.finel.2006.11.011
Autor:
Vijay K. Goyal, Rakesh K. Kapania
Publikováno v:
AIAA Journal. 40:2336-2344
Three models were developed to predict randomness in the free vibration response of unsymmetrically laminated beams: exact Monte Carlo simulation, sensitivity-based Monte Carlo simulation, and probabilistic finite element analysis (FEA). It is assume
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ab3c657cc58b286bfab020f532d7d042
https://doi.org/10.2514/2.1573
https://doi.org/10.2514/2.1573
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Composites materials may exhibit a remarkable difference in material properties depending on whether the state of stress is tension or compression. This tension-compression discontinuity in material properties often leads to a nonconvergent finite el
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36b6c36828a4f0e4edc052b28e67d796
https://doi.org/10.2514/6.2007-2257
https://doi.org/10.2514/6.2007-2257
Publikováno v:
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th.
A model to simulate bird-strike events under various conditions is developed to establish a comparison between the LS-DYNA simulations using the Lagrangian and Smooth Particle Hydrodynamic finite element methods. Classical test data available in the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e587ee89236b2ce862ed2c2c66a2c5fe
https://doi.org/10.2514/6.2006-1759
https://doi.org/10.2514/6.2006-1759
Autor:
Rakesh K. Kapania, Vijay K. Goyal
Publikováno v:
44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Because of the inherent complexity of fiber-reinforced laminated composites, it can be challenging to manufacture composite structures according to their exact design specifications, resulting in unwanted material and geometric uncertainties. Thus th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa047c39e8f9645da968d962182c5b45
https://doi.org/10.2514/6.2003-1914
https://doi.org/10.2514/6.2003-1914