Computational Evaluations of Structural Integrity in Unmanned Aquatic Vehicles Utilizing Various Conventional and Hybrid Composites Using Hydro-Structural Analyses

<div class="section abstract"><div class="htmlview paragraph">This study focuses on developing and deploying an Unmanned Aquatic Vehicle (UAV) capable of underwater travel. The primary objectives of this project are to detect the presence of dimethyl sulfide and toluene, as well as to identify any potential oil leakage in underwater pipelines. The UAV has a maximum operating depth of 300 m below the water surface. The design of this UAV is derived from the natural design of Rhinaancylostoma, an underwater kind of fish. The maximum operational setting for this mission is fixed at a depth of approximately 300 m beneath the surface of the sea, and the choice of this species is suitable for fulfilling the objectives of this undertaking. This technology will mitigate the risk associated with human interaction in inspection processes and has the potential to encompass various other resources in the future. The initial design data of the UAV is determined using analytical processes and verified formulas. The selection of the airfoil is done by comparing numerous options, such as NACA 0006, NACA 0020, and NACA 0024. The comparison investigation shows that the NACA 0008 has a lower coefficient of drag. ANSYS Workbench tool is utilized for executing computational analysis, encompassing hydrodynamic and hydro-structural simulations. An innovative computational molding technique is utilized as a preprocessing step. Structural examination is conducted in a two-step procedure, utilizing eight different materials. The selected materials for analysis are Boron fiber reinforced polymer (BFRP), AS-Carbon fiber reinforced polymer (CFRP), T-300-CFRP, HMS-CFRP, GY-70-CFRP, Kevlar fiber reinforced polymer, E-Glass fiber reinforced polymer (GFRP), and S-GFRP. The solid model of the UAV is subjected to computational analysis under two distinct loading circumstances. This analysis helps in identifying the most effective materials for future examination of the structure utilizing layer model molding in ANSYS ACP software. Afterwards, hybrid composites are prepared with the imposition of advanced fibers, and so the hydro-structural analyses are computed. The hydrodynamic parameters are calculated, and as a result, the structural performance of UAV is monitored. In the end, the most optimal material is chosen for the developed hydrodynamically efficient UAV's construction, to carry out the application efficiently and reliably.</div></div>

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Journal
SAE technical papers on CD-ROM/SAE technical paper series
Published
2025-02-06
DOI
https://doi.org/10.4271/2025-28-0056
Citations
2
Primary Topic
Fluid Dynamics Simulations and Interactions
Type
article
Field-Weighted Citation Impact
2.67
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article

Computational Evaluations of Structural Integrity in Unmanned Aquatic Vehicles Utilizing Various Conventional and Hybrid Composites Using Hydro-Structural Analyses

Arul Prakash Raji, Manikandan Arumugam, Pachagounder Sakthivel, Vijayanandh Raja et al.
2 citations
SAE technical papers on CD-ROM/SAE technical paper series
Fluid Dynamics Simulations and Interactions
2.67
article

Computational Evaluations of Structural Integrity in Unmanned Aquatic Vehicles Utilizing Various Conventional and Hybrid Composites Using Hydro-Structural Analyses

Arul Prakash Raji, Manikandan Arumugam, Pachagounder Sakthivel, Vijayanandh Raja, L. Natrayan, Beena Stanislaus Arputharaj, Senthil Kumar Madasamy, M. Rajendran, Janani Priyadharshini Veeraperumal Senthil Nathan
article en
2 citations

Abstract

<div class="section abstract"><div class="htmlview paragraph">This study focuses on developing and deploying an Unmanned Aquatic Vehicle (UAV) capable of underwater travel. The primary objectives of this project are to detect the presence of dimethyl sulfide and toluene, as well as to identify any potential oil leakage in underwater pipelines. The UAV has a maximum operating depth of 300 m below the water surface. The design of this UAV is derived from the natural design of Rhinaancylostoma, an underwater kind of fish. The maximum operational setting for this mission is fixed at a depth of approximately 300 m beneath the surface of the sea, and the choice of this species is suitable for fulfilling the objectives of this undertaking. This technology will mitigate the risk associated with human interaction in inspection processes and has the potential to encompass various other resources in the future. The initial design data of the UAV is determined using analytical processes and verified formulas. The selection of the airfoil is done by comparing numerous options, such as NACA 0006, NACA 0020, and NACA 0024. The comparison investigation shows that the NACA 0008 has a lower coefficient of drag. ANSYS Workbench tool is utilized for executing computational analysis, encompassing hydrodynamic and hydro-structural simulations. An innovative computational molding technique is utilized as a preprocessing step. Structural examination is conducted in a two-step procedure, utilizing eight different materials. The selected materials for analysis are Boron fiber reinforced polymer (BFRP), AS-Carbon fiber reinforced polymer (CFRP), T-300-CFRP, HMS-CFRP, GY-70-CFRP, Kevlar fiber reinforced polymer, E-Glass fiber reinforced polymer (GFRP), and S-GFRP. The solid model of the UAV is subjected to computational analysis under two distinct loading circumstances. This analysis helps in identifying the most effective materials for future examination of the structure utilizing layer model molding in ANSYS ACP software. Afterwards, hybrid composites are prepared with the imposition of advanced fibers, and so the hydro-structural analyses are computed. The hydrodynamic parameters are calculated, and as a result, the structural performance of UAV is monitored. In the end, the most optimal material is chosen for the developed hydrodynamically efficient UAV's construction, to carry out the application efficiently and reliably.</div></div>

SAE technical papers on CD-ROM/SAE technical paper seriesVol. 1
Rajalakshmi Engineering College, Saveetha University (IN)
Openalex Percentile: Top 14%
Fluid Dynamics Simulations and Interactions
2.67
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