Abstract
The increase in mixing induced by the axial vortices of the cantilevered ramp injector at a high convective Mach number of 1.5 was assessed. The problems investigated are representative of inert mixing occurring in a shcramjet inlet. Results were obtained with the Window Allocatable Resolver for Propulsion (WARP).
| Original language | English (US) |
|---|---|
| Pages (from-to) | 1386-1388 |
| Number of pages | 3 |
| Journal | AIAA journal |
| Volume | 41 |
| Issue number | 7 |
| DOIs | |
| State | Published - Jul 2003 |
| Externally published | Yes |
ASJC Scopus subject areas
- Aerospace Engineering