K. Masania
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16 records found
1
Decoding Signs of Life
Gas-phase FT-IR Analysis of Microbial Biosignature in Simulated Exoplanetary Environments
Hybrid Beam-3D Continuum Nonlinear Modeling of Architected Truss Metamaterials
Insights into Joint Geometry
Previous research has shown that their mechanical performance depends not only on the beams themselves, but also on parameters such as material choice, manufacturing method, lattice architecture, and the shape of the joints where beams meet. This thesis extends existing joint-resolved modeling approaches beyond the linear elastic range into the nonlinear regime, where large deformations and buckling become important. To do so, it develops a hybrid finite element framework in which joints are represented by detailed 3D solid elements and struts by efficient beam elements, combining improved physical realism with manageable computational cost. The thesis presents a nonlinear solver, validation metrics, an accuracy and computational efficiency study, and outlines future developments toward monolithic and data-driven modeling approaches. ...
Previous research has shown that their mechanical performance depends not only on the beams themselves, but also on parameters such as material choice, manufacturing method, lattice architecture, and the shape of the joints where beams meet. This thesis extends existing joint-resolved modeling approaches beyond the linear elastic range into the nonlinear regime, where large deformations and buckling become important. To do so, it develops a hybrid finite element framework in which joints are represented by detailed 3D solid elements and struts by efficient beam elements, combining improved physical realism with manageable computational cost. The thesis presents a nonlinear solver, validation metrics, an accuracy and computational efficiency study, and outlines future developments toward monolithic and data-driven modeling approaches.
Airfoil separation control using tension-activated kirigami metasurfaces
An exploratory aerodynamic investigation into the art of kirigami
A finite element model of the kirigami was validated against laser scans of a vinyl-cut prototype, showing strong agreement in deployment height and successfully highlighting non-uniformity effects. Using rounded rectangular cut-outs on the strip outside the kirigami geometry, both the deployment height and the deployment uniformity were increased. The device was placed between x/c = 0.55 to 0.7 on a DU96 airfoil, with a device height ranging h/δ = 0.1 - 0.3.
PIV measurements showed that at 6–10° angle of attack, separation was aggravated, whereas at 12–14° separation was reduced, with smaller separation regions, weaker reverse flow, and significant drag reduction. At higher angles, the kirigami became submerged in the separation bubble (h/δ = 0.05) and lost effectiveness. Results indicate that the device does not act as a vortex generator. Instead, it is hypothesised that either the kirigami modifies near-surface flow through blockage, causes a reduction of shear stress on the kirigami device, or disrupts backflow structures that drive flow reversal. ...
A finite element model of the kirigami was validated against laser scans of a vinyl-cut prototype, showing strong agreement in deployment height and successfully highlighting non-uniformity effects. Using rounded rectangular cut-outs on the strip outside the kirigami geometry, both the deployment height and the deployment uniformity were increased. The device was placed between x/c = 0.55 to 0.7 on a DU96 airfoil, with a device height ranging h/δ = 0.1 - 0.3.
PIV measurements showed that at 6–10° angle of attack, separation was aggravated, whereas at 12–14° separation was reduced, with smaller separation regions, weaker reverse flow, and significant drag reduction. At higher angles, the kirigami became submerged in the separation bubble (h/δ = 0.05) and lost effectiveness. Results indicate that the device does not act as a vortex generator. Instead, it is hypothesised that either the kirigami modifies near-surface flow through blockage, causes a reduction of shear stress on the kirigami device, or disrupts backflow structures that drive flow reversal.
This research is structured in a three-phase iterative framework. The initial phase involves problem analysis and the development of design specifications. The next phase, material exploration, identifies a list of potential bio-based materials suitable for design exploration, followed by a literature review to understand their flammability and moisture resistance properties, which are critical for compliance with the rigorous standards of aircraft applications.
From the material exploration, a family of hardwood, natural fibers, and mycelium emerged as potential materials for further design exploration. Lightweighting method was employed to optimize their geometry and meet the required mechanical strength established in the design specifications (Load bearing strength up to 100kgs). This method led to the development of a more practical option: the Designing of Composites. Static load-bearing capacity calculations were conducted to assess the feasibility of the composite design with the variations in facesheet materials. The pretreated Baxis Sinica wood panel with a mycelium core emerged as a feasible solution, primarily due to its weight-to-strength ratio, ability to meet the functional requirements of aircraft, and its circularity.
In the pursuit of material optimization, studies were undertaken in exploring bio-based coatings, to enhance the flammability and moisture resistance properties ensuring its suitability for the stringent requirements of aircraft applications. With established research on enhancing the flammability and water resistance of wood-based composites, the focus was to improving the properties of mycelium. Initial post-treatment methods using inorganic flame retardants like sodium silicate effectively demonstrated flame-extinguishing properties; however, further research is required to further enhance the material's water resistance. Additionally, there is promising potential for utilizing bio-based coatings to simultaneously improve both the flame retardancy and moisture resistance of mycelium. As it is well-established that bio-derived materials can degrade over time, it is crucial to develop strategies and treatments to ensure this does not compromise the product's lifespan. Current efforts also focuses on understanding the long-term behavior of these materials and their coatings under extreme conditions. However, as these materials have not yet reached full maturity, further optimization and enhancement remain within the scope of future research.
Positioned within the framework of Circular R-strategies, this study proposes an ambitious design, utilizing a wood and mycelium to develop a composite, with textile serving as the adhesive layer. The proposed design not only eliminates the need for fossil-based materials but also reduces weight by up to 50% compared to conventional thermoplastics in seat trims. This weight reduction is significant, as even a single kilogram less can lead to a decrease of 5,000 to 15,000 kg CO2 emissions over the aircraft's lifetime. ...
This research is structured in a three-phase iterative framework. The initial phase involves problem analysis and the development of design specifications. The next phase, material exploration, identifies a list of potential bio-based materials suitable for design exploration, followed by a literature review to understand their flammability and moisture resistance properties, which are critical for compliance with the rigorous standards of aircraft applications.
From the material exploration, a family of hardwood, natural fibers, and mycelium emerged as potential materials for further design exploration. Lightweighting method was employed to optimize their geometry and meet the required mechanical strength established in the design specifications (Load bearing strength up to 100kgs). This method led to the development of a more practical option: the Designing of Composites. Static load-bearing capacity calculations were conducted to assess the feasibility of the composite design with the variations in facesheet materials. The pretreated Baxis Sinica wood panel with a mycelium core emerged as a feasible solution, primarily due to its weight-to-strength ratio, ability to meet the functional requirements of aircraft, and its circularity.
In the pursuit of material optimization, studies were undertaken in exploring bio-based coatings, to enhance the flammability and moisture resistance properties ensuring its suitability for the stringent requirements of aircraft applications. With established research on enhancing the flammability and water resistance of wood-based composites, the focus was to improving the properties of mycelium. Initial post-treatment methods using inorganic flame retardants like sodium silicate effectively demonstrated flame-extinguishing properties; however, further research is required to further enhance the material's water resistance. Additionally, there is promising potential for utilizing bio-based coatings to simultaneously improve both the flame retardancy and moisture resistance of mycelium. As it is well-established that bio-derived materials can degrade over time, it is crucial to develop strategies and treatments to ensure this does not compromise the product's lifespan. Current efforts also focuses on understanding the long-term behavior of these materials and their coatings under extreme conditions. However, as these materials have not yet reached full maturity, further optimization and enhancement remain within the scope of future research.
Positioned within the framework of Circular R-strategies, this study proposes an ambitious design, utilizing a wood and mycelium to develop a composite, with textile serving as the adhesive layer. The proposed design not only eliminates the need for fossil-based materials but also reduces weight by up to 50% compared to conventional thermoplastics in seat trims. This weight reduction is significant, as even a single kilogram less can lead to a decrease of 5,000 to 15,000 kg CO2 emissions over the aircraft's lifetime.
To facilitate a systematic exploration, this goal was divided into three smaller pieces. Firstly, the study delves into the mechanical characteristics, aiming to identify the most suitable bio-ink crosslink technique and composition. To validate the mechanical properties the living material was subjected to rheology and a bridging test. Concluded can be that crosslinking and algae growth improve the mechanical stability of the material, whereas, gelatin did not. The sagging behaviour of the material looked promising.
Secondly, the photosynthetic activity of this living material was researched. It was found that the rise of O2 levels can not be measured accurately, the non-living matrix can release a high amount of CO2 of over 20.000 ppm and airtightness poses a complex challenge in this field of research.
Lastly, the project incorporates attempts to find effective techniques for studying the livingness of this unique material. In this part of the research, inverted optical microscopy, 3D laser scanning microscopy and chlorophyll extraction were discarded as suitable methods to study the livingness of the algae material. It was proven that leveraging the autofluorescence of the algal chlorophyll confocal laser scanning microscopy gives high-resolution images and the livingness of this living material could be studied with this technique in the near future.
This research significantly contributes to our understanding of this hydrogel-based living material and its many challenging properties. It underscores the importance of innovative materials like these in addressing contemporary environmental challenges, particularly in carbon capture. Moreover, it highlights the complexity of characterizing such materials, paving the way for further exploration and development in this relatively new field. ...
To facilitate a systematic exploration, this goal was divided into three smaller pieces. Firstly, the study delves into the mechanical characteristics, aiming to identify the most suitable bio-ink crosslink technique and composition. To validate the mechanical properties the living material was subjected to rheology and a bridging test. Concluded can be that crosslinking and algae growth improve the mechanical stability of the material, whereas, gelatin did not. The sagging behaviour of the material looked promising.
Secondly, the photosynthetic activity of this living material was researched. It was found that the rise of O2 levels can not be measured accurately, the non-living matrix can release a high amount of CO2 of over 20.000 ppm and airtightness poses a complex challenge in this field of research.
Lastly, the project incorporates attempts to find effective techniques for studying the livingness of this unique material. In this part of the research, inverted optical microscopy, 3D laser scanning microscopy and chlorophyll extraction were discarded as suitable methods to study the livingness of the algae material. It was proven that leveraging the autofluorescence of the algal chlorophyll confocal laser scanning microscopy gives high-resolution images and the livingness of this living material could be studied with this technique in the near future.
This research significantly contributes to our understanding of this hydrogel-based living material and its many challenging properties. It underscores the importance of innovative materials like these in addressing contemporary environmental challenges, particularly in carbon capture. Moreover, it highlights the complexity of characterizing such materials, paving the way for further exploration and development in this relatively new field.
Frontal Polymerization in Fiber Reinforced Polymers
Influence of varying fiber volume fraction and varying geometry
...
The main focus of this work is to optimize a polymer and polymer foaming technique to obtain a high level of porosity, while also retaining adequate mechanical properties. The next step is to achieve a high poling efficiency for the composite in order to obtain good piezoelectric properties. For the polymer system, polyvinyl alcohol (PVA) is selected as the matrix due to its excellent film forming ability as well as its relatively high dielectric properties (compared to polymers). The direct foaming technique is used for this work, due to its simplicity and its reproducibility. For the lead-free ceramic system, Barium Titanate (BaTiO3) and Sodium Potassium Niobate doped with Lithium (KNLN3) is selected as they have good piezoelectric properties, and have been used in piezoelectric composites extensively. As a porous piezoelectric composite is used in this work, the contact poling is replaced by the corona poling method to prevent localized dielectric breakdowns and non-uniform poling.
With the direct foaming technique, foams with porosites in the range of 90-95 % are obtained, resulting in a drastic reduction in the permittivity of the composite. Such a high porosity level also results in a much softer composite. The optimization of the corona poling process is done by selecting the adequate poling temperature and the grid voltage, which is found to be 110 °C and 6 kV respectively. The effective piezoelectric charge coefficient is measured using Al plates as electrodes, to prevent the soft composites from compressing locally. The foam composites exhibit remarkably high g33 values exceeding the 1000 mV.m/N mark, almost double the best sensor used in the industry currently (PVDF). This is attributed to the high poling efficiency and the reduced dielectric permittivity of the composite. This opens up the vast number of possibilities for future systems based on porous structures to be used as sensors which can showcase good piezoelectric properties as well as being more flexible/conformable. ...
The main focus of this work is to optimize a polymer and polymer foaming technique to obtain a high level of porosity, while also retaining adequate mechanical properties. The next step is to achieve a high poling efficiency for the composite in order to obtain good piezoelectric properties. For the polymer system, polyvinyl alcohol (PVA) is selected as the matrix due to its excellent film forming ability as well as its relatively high dielectric properties (compared to polymers). The direct foaming technique is used for this work, due to its simplicity and its reproducibility. For the lead-free ceramic system, Barium Titanate (BaTiO3) and Sodium Potassium Niobate doped with Lithium (KNLN3) is selected as they have good piezoelectric properties, and have been used in piezoelectric composites extensively. As a porous piezoelectric composite is used in this work, the contact poling is replaced by the corona poling method to prevent localized dielectric breakdowns and non-uniform poling.
With the direct foaming technique, foams with porosites in the range of 90-95 % are obtained, resulting in a drastic reduction in the permittivity of the composite. Such a high porosity level also results in a much softer composite. The optimization of the corona poling process is done by selecting the adequate poling temperature and the grid voltage, which is found to be 110 °C and 6 kV respectively. The effective piezoelectric charge coefficient is measured using Al plates as electrodes, to prevent the soft composites from compressing locally. The foam composites exhibit remarkably high g33 values exceeding the 1000 mV.m/N mark, almost double the best sensor used in the industry currently (PVDF). This is attributed to the high poling efficiency and the reduced dielectric permittivity of the composite. This opens up the vast number of possibilities for future systems based on porous structures to be used as sensors which can showcase good piezoelectric properties as well as being more flexible/conformable.
Void formation during RTM
An experimental and analytical study on the influence of bundle porosity on void formation during liquid composite molding in woven fabrics