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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...
| Autores principales: | , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
MDPI
2021
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| 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 |