Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | 12th International Conference on Turbochargers and Turbocharging 2016 |
| Seiten | 303-317 |
| Seitenumfang | 15 |
| ISBN (elektronisch) | 9781510856202 |
| Publikationsstatus | Veröffentlicht - 2016 |
| Veranstaltung | 12th International Conference on Turbochargers and Turbocharging 2016 - London, Großbritannien / Vereinigtes Königreich Dauer: 17 Mai 2016 → 18 Mai 2016 |
Publikationsreihe
| Name | 12th International Conference on Turbochargers and Turbocharging 2016 |
|---|---|
| Band | 2016-May |
Abstract
The influences of back disk cavities on centrifugal compressor aerodynamic losses and axial thrusts are evaluated based on numerical simulations. The influences on compressor performance are found to be negligible. Nevertheless, the consideration of the back disk cavity is necessary for the prediction of axial thrusts and back disk cavity power losses. For this reason, simple analytical equations are proposed for the prediction and the results compared to the numerical simulations. The empirical results show an acceptable agreement concerning pressure prediction at the back disk. To improve the empirical solution, a new approach for the circumferential velocity prediction is introduced.
ASJC Scopus Sachgebiete
- Energie (insg.)
- Feuerungstechnik
- Ingenieurwesen (insg.)
- Fahrzeugbau
Zitieren
- Standard
- Harvard
- Apa
- Vancouver
- BibTex
- RIS
12th International Conference on Turbochargers and Turbocharging 2016. 2016. S. 303-317 (12th International Conference on Turbochargers and Turbocharging 2016; Band 2016-May).
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Low inertia centrifugal compressor wheels
T2 - 12th International Conference on Turbochargers and Turbocharging 2016
AU - Fischer, T.
AU - Rätz, H.
AU - Peters, M.
AU - Seume, J. R.
PY - 2016
Y1 - 2016
N2 - The influences of back disk cavities on centrifugal compressor aerodynamic losses and axial thrusts are evaluated based on numerical simulations. The influences on compressor performance are found to be negligible. Nevertheless, the consideration of the back disk cavity is necessary for the prediction of axial thrusts and back disk cavity power losses. For this reason, simple analytical equations are proposed for the prediction and the results compared to the numerical simulations. The empirical results show an acceptable agreement concerning pressure prediction at the back disk. To improve the empirical solution, a new approach for the circumferential velocity prediction is introduced.
AB - The influences of back disk cavities on centrifugal compressor aerodynamic losses and axial thrusts are evaluated based on numerical simulations. The influences on compressor performance are found to be negligible. Nevertheless, the consideration of the back disk cavity is necessary for the prediction of axial thrusts and back disk cavity power losses. For this reason, simple analytical equations are proposed for the prediction and the results compared to the numerical simulations. The empirical results show an acceptable agreement concerning pressure prediction at the back disk. To improve the empirical solution, a new approach for the circumferential velocity prediction is introduced.
UR - http://www.scopus.com/inward/record.url?scp=85014259552&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85014259552
T3 - 12th International Conference on Turbochargers and Turbocharging 2016
SP - 303
EP - 317
BT - 12th International Conference on Turbochargers and Turbocharging 2016
Y2 - 17 May 2016 through 18 May 2016
ER -