Abstract
The numerical analysis, including chemical reaction of an entire ramjet engine is studied to understand the combustion dynamic characteristics of the Integrated Rocket Ramjet System comprehensively. The results of the previous paper1 are used as the initial conditions for the current calculations so that the ignition transient can be computed with continuity. Various physical processes are investigated systemically, including the flame propagation, flame dynamics, turbulence flame evolution and terminal shock train, modal analysis of the system, and interaction mechanism between the oscillating shock wave in the diffuser and pressure wave resulting from combustion energy using spectral analysis.
| Original language | English |
|---|---|
| Publication status | Published - 2001 |
| Event | 37th Joint Propulsion Conference and Exhibit 2001 - Salt Lake City, UT, United States Duration: 2001 Jul 8 → 2001 Jul 11 |
Conference
| Conference | 37th Joint Propulsion Conference and Exhibit 2001 |
|---|---|
| Country/Territory | United States |
| City | Salt Lake City, UT |
| Period | 01-07-08 → 01-07-11 |
All Science Journal Classification (ASJC) codes
- Energy Engineering and Power Technology
- Aerospace Engineering
- Control and Systems Engineering
- Electrical and Electronic Engineering
- Mechanical Engineering