Numerical analysis experimental tests composite-made is a M.Tech project topic for Aerospace Engineering. It gives students a clear starting point for research, implementation planning, and documentation.
Numerical analysis experimental tests composite-made Project Details
| Abstract |
This research project outlines a comprehensive methodology for evaluating the structural integrity and airworthiness of a composite-made airframe designed for a jet-propelled aerial target. Operating under the stringent guidelines of the European Union Aviation Safety Agency (EASA) CS-VLA airworthiness standards, the study details the systematic determination of critical external loads across the operational flight envelope. A rigorous numerical analysis is executed using finite element methods to assess the strength, stress distribution, and structural integrity of the composite airframe under limit and ultimate load conditions. To validate the computational models, ground static proof-of-compliance tests are conducted, measuring physical deformations and strain distributions under simulated aerodynamic loads. The correlation between numerical simulations
and experimental test results provides a robust framework for verifying that the composite structure can withstand critical flight loads without sustaining permanent deformation. Ultimately, this integrated numerical-experimental approach supports the qualification and type certification process of unmanned aerial systems, ensuring structural safety and operational reliability during high-speed target missions.
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| Reference Paper |
Numerical analysis and experimental tests of the composite-made structure of the jet-propelled aerial target |
| Domain |
Aerospace Engineering |
| Sub-Domain |
Structures & Systems / Aerospace Structures / Composite Airframes |
| PDF Download |
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| Get Help |
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