Influence of Flow Rate Distribution on Combustion Instability of Hypergolic Propellant.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Oct2022, Vol. 9 Issue 10, pN.PAG-N.PAG, 20p
- Subject
COMBUSTION COMBUSTION chambers PROPELLANTS HELMHOLTZ equation ROCKET engines FLOW instability TRANSFER functions - Language
- ISSN
- 22264310