Paper information
- Paper code
- Order
2
- Room
208A
- Title
Computational Investigation of effect of Converging-Diverging Nozzle (C-D Nozzle) on the Performance of Pulse Detonation Engine(PDE)- Effects on Thrust and Inlet Pressure
- abstract
- Session
9. Hypersonic and Combined Cycle Propulsion
- symposium
C4. SPACE PROPULSION SYMPOSIUM
- congress
IAC-13
- Type of presentation
oral
Mr. Linsu Sebastian, University of Petroleum and Energy Studies, India
Dr. Ugur Guven, United States;