Effect of a Roughness Element on the Receptivity of a Hypersonic Boundary Layer over a Blunt Cone Due to Pulse Entropy Disturbance with a Single Frequency

A high-order finite difference method was used to simulate the hypersonic flow field over a blunt cone with different height roughness elements. The unsteady flow field induced by pulse disturbances was analyzed and compared with that under continuous disturbances. The temporal and spatial evolution...

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Detalles Bibliográficos
Autores principales: Wang, Zhenqing, Shi, Mingfang, Tang, Xiaojun, Lv, Hongqing, Xu, Lidan
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2018
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7512923/
https://www.ncbi.nlm.nih.gov/pubmed/33265494
http://dx.doi.org/10.3390/e20060404

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7512923/
https://www.ncbi.nlm.nih.gov/pubmed/33265494
http://dx.doi.org/10.3390/e20060404

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