Aerodynamic analysis toroidal propellers forward is a M.Tech project topic for Aerospace Engineering. It gives students a clear starting point for research, implementation planning, and documentation.
Aerodynamic analysis toroidal propellers forward Project Details
| Abstract |
Recent interest in quieter and more effective systems for aerial propulsion has sparked interest in new designs for propellers. These include toroidal propulsion systems, which feature a unique blade structure. Previous studies have examined these systems and their potential for use in vertical lift or marine propulsion systems; however, many questions remain regarding their effectiveness in forward flight as encountered with fixed-wing aircraft, especially in terms of pertinent advance ratios, airspeeds, and Reynolds numbers. This study aims to fill this void by utilizing Computation Fluid Dynamics (CFD) to examine the aerodynamic characteristics of toroidal propellers configured for low forward flight speed and high RPM operational scenarios. Toward this end, two
different geometric designs for the toroidal propellers were developed based on traditional blade chord and pitch angle distributions associated with Minimum Induced Loss propellers. The aerodynamic performance of each of these designs was evaluated over a wide array of advance ratios from 0.40 to 1.25. Results demonstrate that the designed toroidal propellers can produce significantly greater thrust coefficients and efficiencies when compared to traditional Minimum Induced Loss and toroidal propeller designs.
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| Reference Paper |
Aerodynamic analysis of toroidal propellers in forward flight |
| Domain |
Aerospace Engineering |
| Sub-Domain |
Aerodynamics & Propulsion / Computational Aerodynamics / CFD for Aircraft |
| PDF Download |
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| Get Help |
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