Hybrid Deflection of Spoiler Influencing Radar Cross-Section of Tailless Fighter

With the continuous development of advanced fighters towards tailless and flying wing layouts, diverse control surfaces have become the mainstream design. To study the influence of spoiler control surface on the radar cross-section (RCS) of a tailless fighter, a calculation method is presented. The...

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Detalles Bibliográficos
Autores principales: Zhou, Zeyang, Huang, Jun
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2021
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8709251/
https://www.ncbi.nlm.nih.gov/pubmed/34960556
http://dx.doi.org/10.3390/s21248459

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8709251/
https://www.ncbi.nlm.nih.gov/pubmed/34960556
http://dx.doi.org/10.3390/s21248459

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