ManuScript Details
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Paper Id:
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IJARW3126
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Title:
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CONCEPTUAL DESIGN, AND FEA -BASED STRUCTURAL ANALYSIS OF UNMANNED AERIAL VEHICLE FOR SURVEILLANCE APPLICATIONS
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| Published in: |
International Journal Of All Research Writings |
| Publisher: |
IJARW |
| ISSN: |
2582-1008 |
| Volume / Issue: |
Volume 7 Issue 12 |
| Pages: |
17
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| Published On: |
6/23/2026 8:45:26 PM (MM/dd/yyyy) |
Main Author Details
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Name:
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VURITY YASHOWANTH |
| Institute: |
Visakha Institute of Engineering & Technology |
Co - Author Details
| Author Name |
Author Institute |
| Dr D Santha Rao |
Visakha Institute of Engineering & Technology |
| M RAM BABU |
Visakha Institute of Engineering & Technology |
Abstract
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Research Area:
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Mechanical Engineering |
| KeyWord: |
UAV, fixed-wing drone, surveillance, CFD, structural analysis, modal analysis, composite materials |
| Abstract: |
Unmanned Aerial Vehicles (UAVs) have become important platforms for surveillance because they can perform monitoring tasks with improved operational safety, flexibility, and efficiency. This paper presents the design and simulation-based analysis of a fixed-wing UAV intended for surveillance missions. A conceptual comparison of drone configurations was first carried out, and the fixed-wing configuration was selected because of its superior endurance, aerodynamic efficiency, and suitability for long-range operation. The UAV geometry was developed using calculated aerodynamic design parameters, and the Eppler 387 airfoil was selected for efficient low-speed aerodynamic behavior. Computational Fluid Dynamics (CFD) analysis was conducted to evaluate lift, drag, pressure distribution, velocity behaviour, and aerodynamic moment over different angles of attack, while structural and modal analyses were performed in ANSYS to assess deformation, stress, strain, and vibration response for multiple composite materials [cite:1]. The results indicate that Kevlar 149 fiber epoxy provides the best overall structural stability, lower deformation, and improved vibration resistance among the studied materials, making it suitable for fixed-wing surveillance UAV applications. |
Citations
Copy and paste a formatted citation or use one of the links to import into a bibliography manager and reference.
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IEEE
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VURITY YASHOWANTH, Dr D Santha Rao , M RAM BABU, "CONCEPTUAL DESIGN, AND FEA -BASED STRUCTURAL ANALYSIS OF UNMANNED AERIAL VEHICLE FOR SURVEILLANCE APPLICATIONS", International Journal Of All Research Writings,
vol. 7, no. 12, pp. 120-136, 2026.
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MLA
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VURITY YASHOWANTH, Dr D Santha Rao , M RAM BABU "CONCEPTUAL DESIGN, AND FEA -BASED STRUCTURAL ANALYSIS OF UNMANNED AERIAL VEHICLE FOR SURVEILLANCE APPLICATIONS." International Journal Of All Research Writings,
vol 7, no. 12, 2026, pp. 120-136.
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APA
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VURITY YASHOWANTH, Dr D Santha Rao , M RAM BABU (2026). CONCEPTUAL DESIGN, AND FEA -BASED STRUCTURAL ANALYSIS OF UNMANNED AERIAL VEHICLE FOR SURVEILLANCE APPLICATIONS. International Journal Of All Research Writings,
7(12), 120-136.
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CONCEPTUAL DESIGN, AND FEA -BASED STRUCTURAL ANALYSIS OF UNMANNED AERIAL VEHICLE FOR SURVEILLANCE APPLICATIONS
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