Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | 9th European Conference on Turbomachinery |
| Untertitel | Fluid Dynamics and Thermodynamics, ETC 2011 - Conference Proceedings |
| Herausgeber/-innen | M. Sen, M. Manna, T. Arts, G. Bois |
| Herausgeber (Verlag) | American Society of Mechanical Engineers(ASME) |
| Seiten | 673-682 |
| Seitenumfang | 10 |
| ISBN (elektronisch) | 9789755613901 |
| Publikationsstatus | Veröffentlicht - 1 Jan. 2011 |
| Veranstaltung | 9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011 - Istanbul, Türkei Dauer: 21 März 2011 → 25 März 2011 |
Publikationsreihe
| Name | 9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011 - Conference Proceedings |
|---|---|
| Band | 1 |
| ISSN (Print) | 2410-4833 |
Abstract
Kinetic energy and loss coefficients are presented over a realistic range of swirl angle for an axial annular-conical diffuser with and without tip leakage flow. The analysis of a measured flow field shows that swirl induces the rotation of a recirculation zone downstream of the hub causing additional losses. This study is based on results of experimental investigations conducted in a test rig which is a 1:10 scale model of a typical gas turbine exhaust diffuser. A control volume analysis which applies conservation equations between inlet and outlet of the diffuser is used to evaluate its losses. The flow parameters at the cross sections are averaged values derived by applying the conservation of mean integral characteristics of the real flow, assuming the flow is steady, incompressible, and axisymmetric.
ASJC Scopus Sachgebiete
- Physik und Astronomie (insg.)
- Physik der kondensierten Materie
- Ingenieurwesen (insg.)
- Fahrzeugbau
- Ingenieurwesen (insg.)
- Werkstoffmechanik
- Ingenieurwesen (insg.)
- Maschinenbau
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- BibTex
- RIS
9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011 - Conference Proceedings. Hrsg. / M. Sen; M. Manna; T. Arts; G. Bois. American Society of Mechanical Engineers(ASME), 2011. S. 673-682 (9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011 - Conference Proceedings; Band 1).
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Effect of swirl and tip leakage on flow structure, losses and pressure recovery in axial exhaust diffuser
AU - Sadovnichiy, Victor N.
AU - Kuschel, Marcus
AU - Opilat, Victor
AU - Seume, Joerg R.
PY - 2011/1/1
Y1 - 2011/1/1
N2 - Kinetic energy and loss coefficients are presented over a realistic range of swirl angle for an axial annular-conical diffuser with and without tip leakage flow. The analysis of a measured flow field shows that swirl induces the rotation of a recirculation zone downstream of the hub causing additional losses. This study is based on results of experimental investigations conducted in a test rig which is a 1:10 scale model of a typical gas turbine exhaust diffuser. A control volume analysis which applies conservation equations between inlet and outlet of the diffuser is used to evaluate its losses. The flow parameters at the cross sections are averaged values derived by applying the conservation of mean integral characteristics of the real flow, assuming the flow is steady, incompressible, and axisymmetric.
AB - Kinetic energy and loss coefficients are presented over a realistic range of swirl angle for an axial annular-conical diffuser with and without tip leakage flow. The analysis of a measured flow field shows that swirl induces the rotation of a recirculation zone downstream of the hub causing additional losses. This study is based on results of experimental investigations conducted in a test rig which is a 1:10 scale model of a typical gas turbine exhaust diffuser. A control volume analysis which applies conservation equations between inlet and outlet of the diffuser is used to evaluate its losses. The flow parameters at the cross sections are averaged values derived by applying the conservation of mean integral characteristics of the real flow, assuming the flow is steady, incompressible, and axisymmetric.
UR - http://www.scopus.com/inward/record.url?scp=84915770196&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84915770196
T3 - 9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011 - Conference Proceedings
SP - 673
EP - 682
BT - 9th European Conference on Turbomachinery
A2 - Sen, M.
A2 - Manna, M.
A2 - Arts, T.
A2 - Bois, G.
PB - American Society of Mechanical Engineers(ASME)
T2 - 9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011
Y2 - 21 March 2011 through 25 March 2011
ER -