Study on the effects of nozzle orifice geometry and pulsed injection frequency on transverse jet atomization and total pressure loss in a supersonic crossflow

Autor: Peng, Weidong a, Yin, Bifeng a, ⁎, Yu, Shenghao b, Zhang, Kang a
Zdroj: In Aerospace Science and Technology March 2025 158
Databáze: ScienceDirect