Influence of shock wave/boundary layer interaction on condensation flow and energy recovery in supersonic nozzle.

Autor: Liu, Yang1,2 (AUTHOR), Cao, Xuewen1,2 (AUTHOR), Guo, Dan1,2 (AUTHOR), Cao, Hengguang1,2 (AUTHOR), Bian, Jiang1,2 (AUTHOR) bj@s.upc.edu.cn
Zdroj: Energy. Jan2023:Part A, Vol. 263, pN.PAG-N.PAG. 1p.
Databáze: Academic Search Ultimate