numerical aerodynamic configuration optimisation vtol flying is a M.Tech project topic for Aerospace Engineering. It gives students a clear starting point for research, implementation planning, and documentation.
numerical aerodynamic configuration optimisation vtol flying Project Details
| Abstract |
This research-oriented project framework provides structured guidance for the computational aerodynamic analysis and configuration optimization of a Vertical Take-Off and Landing (VTOL) flying wing unmanned aerial vehicle (UAV). The methodology focuses on evaluating the aerodynamic characteristics of the lifting surface across a broad range of Reynolds numbers (Re โ 9.66 ร 10โด to 1.29 ร 10โถ). Through systematic implementation support, the project guides the development of geometric and computational wing models, grid convergence verification, and the simulation of airflow regimes at various angles of attack (AOA). The numerical framework utilizes the unsteady Reynolds-averaged Navier-Stokes (URANS) equations coupled with a Low Reynolds k-ฮต turbulence model solved via the finite volume method.
Key evaluation metrics include the determination of aerodynamic coefficients, construction of aerodynamic polars, assessment of energy efficiency, and analysis of stability transitions, including ground effect phenomena. This structured research direction assists postgraduate students in understanding the complex flow physics of flying wing configurations, offering a robust foundation for aerodynamic optimization and design refinement of next-generation VTOL UAVs.
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| Reference Paper |
Numerical Investigation and Aerodynamic Configuration Optimisation of a VTOL Flying Wing UAV |
| Domain |
Aerospace Engineering |
| Sub-Domain |
Aerodynamics & Propulsion / Computational Aerodynamics / UAV Aerodynamics |
| PDF Download |
Download / View PDF |
| Get Help |
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