Logesh Shanmugam
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Research Subjects
Logesh Shanmugam has a total of 48 co-authors. Here are the top co-authors by number of shared publications:
- Jinglei Yang
Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Kowloon, Hong Kong
8 shared publications Jinglei Yang
Department of Mechanical and Aerospace Engineering, Hong Kong University of Science and Technology, Hong Kong SAR, P. R. China
7 shared publications- M. Erfan Kazemi
The Chinese University of Hong Kong
7 shared publications Lei Yang
6 shared publicationsShanyi Du
3 shared publicationsBowei Wang
2 shared publications
Latest Publications
- 1 January 2025
- Published by Society for the Advancement of Material and Process Engineering - SAMPE
ENCAPSULATED LOW-OUTGASSING COMPOSITE MANUFACTURING WITH POTENTIAL FOR ON-ORBIT DEMONSTRATION
The future of space exploration requires a paradigm shift from deployable pre-manufactured structures to structures that are manufactured and assembled on-orbit. A demonstration of onorbit manufacturing of high stiffness carbon fiber composites is sought. However, space-based composite manufacturing is significantly constrained by launch volume, on-orbit processing energy and equipment, and off-gassing requirements. While others have used on-orbit thermoplastic additive manufacturing, this study investigates the processing and properties of encapsulated thermoset carbon fiber prepreg with the potential for on-orbit manufacturing of composite tubes. Specifically, we infuse catalyzed dicyclopentadiene (DCPD) resin into layered cylindrical carbon fiber preform sleeves, seal and encapsulate the prepregs between compliant and impermeable films, and then mold and cure the prepreg to rapidly produce a thin-walled, high-stiffness composite tubes using a low energy process with low outgassing. We demonstrate the scalability of tube prepreg by infusing a 10-foot long prepreg with industrial partners. Using flat surrogates of the cylindrical laminate, we demonstrate that the prepregs are stable and can be cured quickly (~ 5 minutes) and with only 11 psi (75.8 Kpa) of applied pressure to create composites with high (155-160°C), low voids (<1%), and low off-gassing (<1%). Initial promise is demonstrated for a future planned space demonstration on the International Space Station (ISS) through “Mission Illinois”.
- 1 January 2025
- Published by Society for the Advancement of Material and Process Engineering - SAMPE
ENCAPSULATED LOW-OUTGASSING COMPOSITE MANUFACTURING WITH POTENTIAL FOR ON-ORBIT DEMONSTRATION
The future of space exploration requires a paradigm shift from deployable pre-manufactured structures to structures that are manufactured and assembled on-orbit. A demonstration of onorbit manufacturing of high stiffness carbon fiber composites is sought. However, space-based composite manufacturing is significantly constrained by launch volume, on-orbit processing energy and equipment, and off-gassing requirements. While others have used on-orbit thermoplastic additive manufacturing, this study investigates the processing and properties of encapsulated thermoset carbon fiber prepreg with the potential for on-orbit manufacturing of composite tubes. Specifically, we infuse catalyzed dicyclopentadiene (DCPD) resin into layered cylindrical carbon fiber preform sleeves, seal and encapsulate the prepregs between compliant and impermeable films, and then mold and cure the prepreg to rapidly produce a thin-walled, high-stiffness composite tubes using a low energy process with low outgassing. We demonstrate the scalability of tube prepreg by infusing a 10-foot long prepreg with industrial partners. Using flat surrogates of the cylindrical laminate, we demonstrate that the prepregs are stable and can be cured quickly (~ 5 minutes) and with only 11 psi (75.8 Kpa) of applied pressure to create composites with high (155-160°C), low voids (<1%), and low off-gassing (<1%). Initial promise is demonstrated for a future planned space demonstration on the International Space Station (ISS) through “Mission Illinois”.
- 6 November 2024
- Published by Elsevier in Composites Communications
- Vol. 52
Flexural behaviours and heterogeneous interface fracture in overmoulded multi-material thermoplastic composites
- 6 November 2024
- Published by Elsevier in Composites Communications
- Vol. 52
Flexural behaviours and heterogeneous interface fracture in overmoulded multi-material thermoplastic composites
- 1 January 2022
- Published by Elsevier in Composite Structures
- Vol. 279
An even-load-distribution design for composite bolted joints using a novel circuit model and neural network
- 1 January 2022
- Published by Elsevier in Composite Structures
- Vol. 279
An even-load-distribution design for composite bolted joints using a novel circuit model and neural network
- 1 March 2021
- Published by World Scientific Pub Co Pte Ltd in Journal of Micromechanics and Molecular Physics
- Vol. 06 (01)
Machine learning-based prediction of the translaminar R-curve of composites from simple tensile test of pre-cracked samples
A novel approach to determine the translaminar crack resistance curve of composite laminates by means of a machine learning model is presented in this paper. The main objective of the proposed method is to extract hidden information of crack resistance from strength values of center-cracked laminates. Compared to traditional measurements, the notable advantage is that only tensile strength values are required which can be obtained by a rather simpler experimental procedure. This is achieved by the incorporation of the finite fracture mechanics, which links crack resistance with strength values. In order to get training dataset, a semi-analytical method using both finite element method and finite fracture mechanics is employed to generate strength values of center-cracked specimens with different random R-curves, which serve as inputs for our artificial neural network. Regarding the outputs, principal component analysis is performed to reduce dimensionality and find suitable descriptors for crack resistance curves. After successfully training machine learning model, experimental studies on basalt fiber reinforced laminates are conducted as validation. Results have proven the effectiveness of the proposed strategy for predicting crack resistance curves, as well as the feasibility of using machine learning-based framework to find out more information about composites from simple experimental data.
- 1 March 2021
- Published by World Scientific Pub Co Pte Ltd in Journal of Micromechanics and Molecular Physics
- Vol. 06 (01)
Machine learning-based prediction of the translaminar R-curve of composites from simple tensile test of pre-cracked samples
A novel approach to determine the translaminar crack resistance curve of composite laminates by means of a machine learning model is presented in this paper. The main objective of the proposed method is to extract hidden information of crack resistance from strength values of center-cracked laminates. Compared to traditional measurements, the notable advantage is that only tensile strength values are required which can be obtained by a rather simpler experimental procedure. This is achieved by the incorporation of the finite fracture mechanics, which links crack resistance with strength values. In order to get training dataset, a semi-analytical method using both finite element method and finite fracture mechanics is employed to generate strength values of center-cracked specimens with different random R-curves, which serve as inputs for our artificial neural network. Regarding the outputs, principal component analysis is performed to reduce dimensionality and find suitable descriptors for crack resistance curves. After successfully training machine learning model, experimental studies on basalt fiber reinforced laminates are conducted as validation. Results have proven the effectiveness of the proposed strategy for predicting crack resistance curves, as well as the feasibility of using machine learning-based framework to find out more information about composites from simple experimental data.
- 10 December 2020
- Published by American Chemical Society (ACS) in ACS Applied Materials & Interfaces
- Vol. 12 (51) , 57547-57559
Robust Microcapsules with Durable Superhydrophobicity and Superoleophilicity for Efficient Oil–Water Separation
The poor ultraviolet (UV) resistance and insufficient solvent compatibility are challenges for long-term storage and service of oil–water separation materials in practical applications. Herein, a superhydrophobic/superoleophilic surface with nano- to microscale hierarchical structures was formed spontaneously on robust microcapsules (MCs) via in situ polymerization and a sol–gel surface treatment. The resultant MCs possessed superior UV-resistant and solvent-proof superhydrophobicity. The water contact angles (WCAs) of the MC coating remained above 160° and the sliding angles (SAs) were below 3° after 9 days of UV aging test or 20 days of nonpolar and polar aprotic solvent immersion tests. More interestingly, these MCs can be used to separate the oil phase from its aqueous emulsion effectively, achieving a high and reusable separation efficiency with over 90% oil purity after 10 cycles of filtrations even after 13 days of UV aging. Therefore, these novel MCs will exhibit effective oil–water separation performance, superior chemical stability, outstanding reusability, and long-term storage stability for promising practical applications.
- 10 December 2020
- Published by American Chemical Society (ACS) in ACS Applied Materials & Interfaces
- Vol. 12 (51) , 57547-57559
Robust Microcapsules with Durable Superhydrophobicity and Superoleophilicity for Efficient Oil–Water Separation
The poor ultraviolet (UV) resistance and insufficient solvent compatibility are challenges for long-term storage and service of oil–water separation materials in practical applications. Herein, a superhydrophobic/superoleophilic surface with nano- to microscale hierarchical structures was formed spontaneously on robust microcapsules (MCs) via in situ polymerization and a sol–gel surface treatment. The resultant MCs possessed superior UV-resistant and solvent-proof superhydrophobicity. The water contact angles (WCAs) of the MC coating remained above 160° and the sliding angles (SAs) were below 3° after 9 days of UV aging test or 20 days of nonpolar and polar aprotic solvent immersion tests. More interestingly, these MCs can be used to separate the oil phase from its aqueous emulsion effectively, achieving a high and reusable separation efficiency with over 90% oil purity after 10 cycles of filtrations even after 13 days of UV aging. Therefore, these novel MCs will exhibit effective oil–water separation performance, superior chemical stability, outstanding reusability, and long-term storage stability for promising practical applications.
- 23 November 2020
- Published by Springer Nature in Advanced Composites and Hybrid Materials
- Vol. 3 (4) , 508-521
Influence of UHMWPE fiber and Ti6Al4V metal surface treatments on the low-velocity impact behavior of thermoplastic fiber metal laminates
- 23 November 2020
- Published by Springer Nature in Advanced Composites and Hybrid Materials
- Vol. 3 (4) , 508-521
Influence of UHMWPE fiber and Ti6Al4V metal surface treatments on the low-velocity impact behavior of thermoplastic fiber metal laminates
- 1 October 2020
- Published by Elsevier in Composite Structures
- Vol. 250
Low-velocity impact behaviors of a fully thermoplastic composite laminate fabricated with an innovative acrylic resin
- 1 October 2020
- Published by Elsevier in Composite Structures
- Vol. 250
Low-velocity impact behaviors of a fully thermoplastic composite laminate fabricated with an innovative acrylic resin