Specific impulse gain mechanism of swirling helium-injected solid–gas hybrid rocket motor
Year: 2025
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0257788
Authors: Zenan Yang, Hao Wang, Chengke Li, Haiwei Yang, Ge Wang
Institution: Harbin Engineering University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4408448448
