Abstract
Fluid structure for the jet impinging upon a flat plate with fields has been investigated at different angles of impingement. The investigation was carried both for jet with Reynolds number of 2750. The numerical simulation was carried over the water jet impingement using hybrid turbulence modeling. The SGS model reduces to k-epsilon model near the walls. The solution was based on the finite volume method called Arbitrary Lagrangian-Eulerian method. Spatial differences were formed on a finite-difference mesh that subdivides the computational region. Water was injected on to the flat plate from a solid cone micro nozzle of cone angle 20°. The distance between the nozzle and the flat plate was 0.1cm. Nozzle plate spacing ratio H/d =10.
| Original language | English |
|---|---|
| Title of host publication | Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting |
| Pages | 15521-15529 |
| Number of pages | 9 |
| Publication status | Published - 2006 Dec 1 |
| Event | 44th AIAA Aerospace Sciences Meeting 2006 - Reno, NV, United States Duration: 2006 Jan 9 → 2006 Jan 12 |
Publication series
| Name | Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting |
|---|---|
| Volume | 20 |
Other
| Other | 44th AIAA Aerospace Sciences Meeting 2006 |
|---|---|
| Country | United States |
| City | Reno, NV |
| Period | 06/1/9 → 06/1/12 |
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All Science Journal Classification (ASJC) codes
- Space and Planetary Science
- Aerospace Engineering
Cite this
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Behavior of Fluid Structure for the Jet Impinging on a Flat Plate. / Kondaraju, S.; Kim, Y. H.; Lee, Joon Sang.
Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. 2006. p. 15521-15529 (Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting; Vol. 20).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
TY - GEN
T1 - Behavior of Fluid Structure for the Jet Impinging on a Flat Plate
AU - Kondaraju, S.
AU - Kim, Y. H.
AU - Lee, Joon Sang
PY - 2006/12/1
Y1 - 2006/12/1
N2 - Fluid structure for the jet impinging upon a flat plate with fields has been investigated at different angles of impingement. The investigation was carried both for jet with Reynolds number of 2750. The numerical simulation was carried over the water jet impingement using hybrid turbulence modeling. The SGS model reduces to k-epsilon model near the walls. The solution was based on the finite volume method called Arbitrary Lagrangian-Eulerian method. Spatial differences were formed on a finite-difference mesh that subdivides the computational region. Water was injected on to the flat plate from a solid cone micro nozzle of cone angle 20°. The distance between the nozzle and the flat plate was 0.1cm. Nozzle plate spacing ratio H/d =10.
AB - Fluid structure for the jet impinging upon a flat plate with fields has been investigated at different angles of impingement. The investigation was carried both for jet with Reynolds number of 2750. The numerical simulation was carried over the water jet impingement using hybrid turbulence modeling. The SGS model reduces to k-epsilon model near the walls. The solution was based on the finite volume method called Arbitrary Lagrangian-Eulerian method. Spatial differences were formed on a finite-difference mesh that subdivides the computational region. Water was injected on to the flat plate from a solid cone micro nozzle of cone angle 20°. The distance between the nozzle and the flat plate was 0.1cm. Nozzle plate spacing ratio H/d =10.
UR - http://www.scopus.com/inward/record.url?scp=34250775617&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=34250775617&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:34250775617
SN - 1563478072
SN - 9781563478079
T3 - Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
SP - 15521
EP - 15529
BT - Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
ER -