- Vortex Shedding Influence on Hybrid Rocket Pressure Oscillations and Combustion Efficiency.
Article
CID:
Authors:
Issue Date:
- November-December 2016
Journal Title:
Issue No.:
- 32
Issue number:
- 6
Collation:
- 1386-1394
Subjects:
Fiction:
- 0
Abstract:
- Numerical simulation is performed and compared with a firing test of a polyethylene hybrid rocket engine equipped with a catalyzer.
Notes:
- Read More: https://arc.aiaa.org/doi/abs/10.2514/1.B36049
Record Type:
- Article