Back to Search
Start Over
Active Control of Dual-Bell Nozzle Operation Mode Transition by Film Cooling and Mixture Ratio Variation
- Source :
- Journal of Propulsion and Power. 36:47-58
- Publication Year :
- 2020
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2020.
-
Abstract
- A numerical study is conducted to investigate the impact of a film-cooled dual-bell nozzle extension on its operation mode transition behavior. Therefore, unsteady Reynolds-averaged Navier–Stokes s...
- Subjects :
- Propellant
Materials science
Mechanical Engineering
Nozzle
nozzle flow
Mathematics::Analysis of PDEs
film cooling
Aerospace Engineering
Mechanics
Regenerative cooling (rocket)
Boundary layer thickness
dual bell nozzle
Physics::Fluid Dynamics
Hysteresis
Fuel Technology
Space and Planetary Science
Bell nozzle
Combustion chamber
Reynolds-averaged Navier–Stokes equations
Subjects
Details
- ISSN :
- 15333876
- Volume :
- 36
- Database :
- OpenAIRE
- Journal :
- Journal of Propulsion and Power
- Accession number :
- edsair.doi.dedup.....4c59550891341cb2b62036be5a0061a5