Limits of high-pressure hydrogen jet combustion in argon power cycle-based energy systems
Abstract
• H 2 jet ignition in argon cycle studied on powerplant-relevant engine setup. • 1D system-in-the-loop CFD resolves full power cycle. • Liner/piston confinement suppresses jet momentum, limiting H 2 –O 2 mixing. • Increasing injection rate helps mixing but is limited by peak pressure. • Unburned H 2 must stay
Fields of Study & Subjects
Combustion and flame dynamics
Advanced Combustion Engine Technologies
Combustion and Detonation Processes
Publication details
- Journal / source
- Fuel
- Publisher
- Elsevier BV
- Volume
- 426
- Pages
- 139603–139603
- Publication date
- 25 April 2026
- Language
- EN