Research on control effectiveness of fluidic thrust vectoring

In view of the control effects of fluidic thrust vector technology for low-speed aircraft at high altitude/low density and low altitude/high density are studied. The S-A model of FLUENT software is used to simulate the flow field inside and outside the nozzle with variable control surface parameters...

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Detalles Bibliográficos
Autores principales: Xue, Fei, Yunsong, Gu, Wang, Yuchao, Qin, Han
Formato: Online Artículo Texto
Lenguaje:English
Publicado: SAGE Publications 2021
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10453779/
https://www.ncbi.nlm.nih.gov/pubmed/33719731
http://dx.doi.org/10.1177/0036850421998137

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10453779/
https://www.ncbi.nlm.nih.gov/pubmed/33719731
http://dx.doi.org/10.1177/0036850421998137

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