Flight/Propulsion Integrated Control of Over-Under TBCC Engine Based on GA-LQR Method.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Oct2022, Vol. 9 Issue 10, pN.PAG-N.PAG, 13p
- Subject
MACH number TRANSITION flow AIRPLANE motors SHOCK waves ENGINES ELECTRIC propulsion HYPERSONIC planes - Language
- ISSN
- 22264310