Numerical investigation on thrust gain mechanism of helium injected solid–gas hybrid rocket motor | Citedby Results | Physics of Fluids | AIP Publishing

Skip to Main Content

Skip Nav Destination

Numerical investigation on thrust gain mechanism of helium injected solid–gas hybrid rocket motor

Physics of Fluids 36, 096121 (2024)

This article has been cited by the following articles in journals that are participating in CrossRef Cited-by Linking.

Specific impulse gain mechanism of swirling helium-injected solid–gas hybrid rocket motor

Zenan Yang
Hao Wang
Chengke Li
Haiwei Yang
Ge Wang

Physics of Fluids (2025) 37 (3)