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Autor:
Panneerselvam Padmanathan, Seenu Aswin, Anbalagan Satheesh, Parthasarathy Rajesh Kanna, Kuppusamy Palani, Neelamegam Rajan Devi, Tomasz Sobota, Dawid Taler, Jan Taler, Bohdan Węglowski
Publikováno v:
Applied Sciences, Vol 14, Iss 17, p 7483 (2024)
This paper deals with the topic of reducing drag force acting on aircraft wings by incorporating novel winglet designs, such as multi-tip, bird-type, and twisted. The high-speed NASA common research model (CRM) was selected as the baseline model, and
Externí odkaz:
https://doaj.org/article/e7a344ab05b84e8c9c3b1a0a726ff79c