 |
Tubular burner. |
|
Periodic stretch counterflow diffusion flame burner. |
Rendered Images of Burners
|
Vanderbilt's counterflow burner, based on Seshadri's design. |
|
Vanderbilt's lean premixed combustor, provided by Wright Laboratories. |
|
Vanderbilt's co-flow burner, created from the lean premixed combustor. |
|
Cross section view of the co-flow burner. |
|
Vanderbilt's tubular flame burner. Laser beam travels through window extensions, while scattered light is collected through a perpendicular window. |
|
Close-up view of the tubular flame burner. |
|
Cross section view of the tubular flame burner. Air enters the burner through 16 evenly-spaced air inlet ports (8 on the top, 8 on the bottom) and travels radially inward. The fuel is injected into a central cintered brass tube and travels radially outward. In this manner, a tubular flame is stabilized inside the burner. |