University of Illinois at Urbana-Champaign
An Experimental Investigation Into the Effect of Plasma on the Flow Features of an Axisymmetric Jet
Abstract
dc:descriptionThe plasma did influence the mean and turbulent velocity profiles of the jets tested - allowing the jet core to penetrate further downstream. Large scale structure tracking indicated an increase in convective velocity of up to 5%. Heating of the shear layer by the plasma field was believed to bias the convective velocity towards the jet core by increasing the speed of sound in the shear layer. Rotational temperatures taken by model matching of spectroscopy data indicated shear layer heating which supports an equivalent increase in convective velocity as was measured in large scale structure tracking. In perfectly expanded jets, turbulent kinetic energy decreased along the jet centerline by 7% to 14% and were not influenced by compressibility which is consistent with increased jet penetration. However, in pipe-flow jets the centerline turbulent kinetic energy decreased at low equivalent Mach numbers, reversing to slight increases for equivalent Mach numbers over 1.4.
Degree
thesis:*- Name thesis:degree_name
- Ph.D.
- Level thesis:degree_level
- Dissertation
- Discipline thesis:degree_discipline
- Aerospace Engineering
- Grantor
- University of Illinois at Urbana-Champaign
- Year dc:date
- 2015
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Huffman, Richard E.
- Contributors dc:contributor
-
- Gregory Elliott
Subjects
dc:subject × 1Rights
- Language dc:language
- eng
Identifiers
dc:identifier.*- Identifier
- (MiAaPQ)AAI3301152
- OAI identifier oai:identifier
- oai:www.ideals.illinois.edu:2142/85105