Abstract
Global mode decomposition is applied to high speed jets over a range of jet-to-ambient density ratios and Mach numbers. Maximal transient response was obtained for each system by computing an optimal superposition of non-normal global modes. The non-normality of the global modes increased with decreasing density ratio as well as decreasing Mach number.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 285-302 |
| Number of pages | 18 |
| Journal | International Journal of Spray and Combustion Dynamics |
| Volume | 3 |
| Issue number | 4 |
| DOIs | |
| State | Published - Dec 1 2011 |