Numerical investigation on thrust gain mechanism of helium injected solid–gas hybrid rocket motor
Year: 2024
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0230517
Authors: Chengke Li, Ge Wang, Hao Wang, Weijie Zhang, Ben Guan, Haiwei Yang, Zenan Yang
Institution: Harbin Engineering University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G6568785768, G739764700
OpenAlex ID: W4402682401