Structure of a supersonic separated flow over a compression corner with side walls

Autor:	L. P. Trubitsyna, I. N. Kavun, V. I. Zapryagaev
Rok vydání:	2021
Předmět:	Materials science Transversal (combinatorics) Line (geometry) Flow (psychology) Geometry Supersonic speed Total pressure Compression (physics) Layer (electronics) Freestream
Zdroj:	AIP Conference Proceedings.
ISSN:	0094-243X
DOI:	10.1063/5.0052018
Popis:	The work focuses on the effect of transversal runoff on the high-pressure layer in a supersonic (M = 6) separated compression corner flow. The high-pressure layer is formed behind the reattachment line of the separated flow and is characterized by high values of total pressure (90-95% of the freestream total pressure). The presented experimental results show that the high-pressure layer exists in a flow without transversal runoff.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::319de3f4c75854b72c24e8c9aacb36da https://doi.org/10.1063/5.0052018 Zobrazit plný text záznamu