Design and Multi-Perspective based Computational Analyses of Flying Wing UAV for Rescue Applications at Cryogenic Environments-Reference-Cited by-同舟云学术

Design and Multi-Perspective based Computational Analyses of Flying Wing UAV for Rescue Applications at Cryogenic Environments

Published:2022-06-20 Issue: Volume: Page:
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Container-title:AIAA AVIATION 2022 Forum
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Author:

Raja Vijayanandh¹,Prabhu Manikandan¹,Murugan Karthikeyan¹,Solaiappan Senthil Kumar¹,Raji Arul Prakash¹,Gnanasekaran Raj Kumar¹,Ramaiah Manivel¹,Rajapandi Rajkumar¹,Mathaiyan Vijayakumar¹,Nandhan Akshay Kumar¹,Kannan Aswathama¹

Affiliation:

1. Kumaraguru College of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3586

Reference31 articles.

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2. Prasetyo Edi, Nukman Yusoff and Aznijar Ahmad Yazid, Airfoil Design for Flying Wing UAV (Unmanned Aerial Vehicle), Proceedings of the 4th WSEAS International Conference on applied and theoretical mechanics (MECHANICS '08), ISSN: 1790-2769, ISBN: 978-960-474-046-8,106 - 111. 2008.

3. Kamal AM, Ramirez-Serrano A. Design methodology for hybrid (VTOL + Fixed Wing) unmanned aerial vehicles. Aeron Aero Open Access J. 2018;2(3):165-176. DOI: 10.15406/aaoaj.2018.02.0004710.15406/aaoaj.2018.02.00047

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