Materials Map

Discover the materials research landscape. Find experts, partners, networks.

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The Materials Map is an open tool for improving networking and interdisciplinary exchange within materials research. It enables cross-database search for cooperation and network partners and discovering of the research landscape.

The dashboard provides detailed information about the selected scientist, e.g. publications. The dashboard can be filtered and shows the relationship to co-authors in different diagrams. In addition, a link is provided to find contact information.

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Materials Map under construction

The Materials Map is still under development. In its current state, it is only based on one single data source and, thus, incomplete and contains duplicates. We are working on incorporating new open data sources like ORCID to improve the quality and the timeliness of our data. We will update Materials Map as soon as possible and kindly ask for your patience.

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in Cooperation with on an Cooperation-Score of 37%

Topics

Publications (2/2 displayed)

  • 2024Design, control, aerodynamic performances, and structural integrity investigations of compact ducted drone with co-axial propeller for high altitude surveillance13citations
  • 2023Comprehensive computational investigations on various aerospace materials under complicated loading conditions through conventional and advanced analyses: a verified examination2citations

Places of action

Chart of shared publication
Stanislaus Arputharaj, Beena
1 / 1 shared
Rajendran, Parvathy
2 / 2 shared
Madasamy, Senthil Kumar
1 / 1 shared
Subramaniam, Indira Prasanth
1 / 1 shared
Jayakumar, S.
1 / 2 shared
Arunkumar, K.
1 / 2 shared
Lee, It Ee
1 / 1 shared
Senthil Kumar, S.
1 / 2 shared
Raja, Vijayanandh
1 / 1 shared
Shanmugam, Balasubramanian
1 / 1 shared
Radhakrishnan, Jeeva
1 / 1 shared
Al-Bonsrulah, Hussein A. Z.
1 / 1 shared
Narayanan, Venkatesh
1 / 1 shared
Eldin, Sayed M.
1 / 9 shared
Chart of publication period
2024
2023

Co-Authors (by relevance)

  • Stanislaus Arputharaj, Beena
  • Rajendran, Parvathy
  • Madasamy, Senthil Kumar
  • Subramaniam, Indira Prasanth
  • Jayakumar, S.
  • Arunkumar, K.
  • Lee, It Ee
  • Senthil Kumar, S.
  • Raja, Vijayanandh
  • Shanmugam, Balasubramanian
  • Radhakrishnan, Jeeva
  • Al-Bonsrulah, Hussein A. Z.
  • Narayanan, Venkatesh
  • Eldin, Sayed M.
OrganizationsLocationPeople

article

Comprehensive computational investigations on various aerospace materials under complicated loading conditions through conventional and advanced analyses: a verified examination

  • Raja, Vijayanandh
  • Shanmugam, Balasubramanian
  • Rajendran, Parvathy
  • Gnanasekaran, Raj Kumar
  • Radhakrishnan, Jeeva
  • Al-Bonsrulah, Hussein A. Z.
  • Narayanan, Venkatesh
  • Eldin, Sayed M.
Abstract

<jats:p>Most failures develop as a result of a lack of resistivity information at the internal structure level during typical loading situations such as shock load and impact load. Impact loads have a significant impact on a component’s structural performance. A careful, organized examination of impact load settings and their side effects can reveal how well something can withstand peak loads. First, this study investigated the impact analyses on nine varied lightweight composite materials through a conventional experimental setup and computational tools. So, the best three lightweight materials are shortlisted for further investigation under complicated explicit analysis. Second, the study investigated the behavior of composite materials subjected to rapid loading circumstances in several real-time applications. The applications chosen include bullet crash analysis, unmanned aerial vehicle (UAV) propellers, and car bumpers. The three different principal composites, carbon fiber-reinforced polymer (CFRP), glass fiber-reinforced polymer (GFRP), and Kevlar fiber-reinforced polymer (KFRP), are selected and applied in crash analysis using ANSYS Workbench’s explicit technique-based finite element analysis (FEA). The comparison assessments are conducted using stumpy structural characteristics such as impact stress and equivalent strain. Two distinct grid convergence tests were performed to check whether the computational processes and discretization were correct. The standard methodologies were used on all three selected real-time applications, resulting in error percentages that were within acceptable bounds, ensuring the generation of dependable structural outputs. The ideal composite material is a Kevlar fiber-based composite with minimal defect affectability for all types of crash applications. Furthermore, multidisciplinary optimizations are performed, and the KFRP is verified to give good crash load resistance with reduced dense contribution.</jats:p>

Topics
  • impedance spectroscopy
  • polymer
  • Carbon
  • resistivity
  • glass
  • glass
  • composite
  • defect
  • finite element analysis