Computational investigations for the application of winglets on small-scale UAVs
Author:
Affiliation:
1. Institute of Aeronautics, Riga Technical University,Faculty of Mechanical Engineering, Transport, and Aeronautics,Riga,Latvia
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10171240/10171198/10171275.pdf?arnumber=10171275
Reference18 articles.
1. A simplified design approach for high-speed wind tunnels. Part II: Diffuser optimization and complete duct design;arshad;Journal of Mechanical Science and Technology,2020
2. A Simplified Design Approach for High-Speed Wind Tunnels. Part-I.I: Optimized Design of Settling Chamber and Inlet Nozzle
3. Stability Analysis for a Concept Design of Vertical Take-off and Landing (VTOL) Unmanned Aerial Vehicle (UAV)
4. Computational Study of Noise Reduction in CFM56-5B Using Core Nozzle Chevrons
5. A simplified design approach for high-speed wind tunnels. Part I: Table of inclination
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2. Application of SG6043mod Airfoil for the Enhanced Aerodynamic Characteristics of UAV Wing;2023 10th International Conference on Recent Advances in Air and Space Technologies (RAST);2023-06-07
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