Details
| Originalsprache | Englisch |
|---|---|
| Seiten (von - bis) | 233-247 |
| Seitenumfang | 15 |
| Fachzeitschrift | International Journal of Turbo and Jet Engines |
| Jahrgang | 19 |
| Ausgabenummer | 4 |
| Publikationsstatus | Veröffentlicht - 1 Dez. 2002 |
| Veranstaltung | Tagung: Turbokompressoren im industriellen Einsatz - Duisburg, Deutschland Dauer: 18 Sept. 2002 → 19 Sept. 2002 |
Abstract
The correlation between the frequencies of pressure oscillation ωosc and the rotor speed (frequencies of rotor rotation ωRR) under established rotating stall were determined by three methods: directly from the time diagram of the oscillation process, from the behavior diagram of parameters in space and time and from frequency characteristics. In total accordance with the Theory of Nonlinear Oscillation, by all methods of analysis, the links are in the form of integer ratios: ωosc / ωRR = 1:2 (for n/ nd= 0.6, where n - rotor speed in the experiment and nd- rotor speed from data-sheet) and ωosc / ωRR = 3:7 (for n/ nd = 0.8 and 0.95). The phases of parameter oscillations in the transverse cross-section are equal to the sensor angles in compressor stator. This is in agreement with the theoretical concept of single-cell configurations of rotating stall.
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- Luft- und Raumfahrttechnik
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in: International Journal of Turbo and Jet Engines, Jahrgang 19, Nr. 4, 01.12.2002, S. 233-247.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - Relationship between Frequencies of Pressure Oscillations and Rotor Speed under Rotating Stall
AU - Levy, Y.
AU - Pismenny, J.
AU - Reissner, A.
AU - Riess, W.
PY - 2002/12/1
Y1 - 2002/12/1
N2 - The correlation between the frequencies of pressure oscillation ωosc and the rotor speed (frequencies of rotor rotation ωRR) under established rotating stall were determined by three methods: directly from the time diagram of the oscillation process, from the behavior diagram of parameters in space and time and from frequency characteristics. In total accordance with the Theory of Nonlinear Oscillation, by all methods of analysis, the links are in the form of integer ratios: ωosc / ωRR = 1:2 (for n/ nd= 0.6, where n - rotor speed in the experiment and nd- rotor speed from data-sheet) and ωosc / ωRR = 3:7 (for n/ nd = 0.8 and 0.95). The phases of parameter oscillations in the transverse cross-section are equal to the sensor angles in compressor stator. This is in agreement with the theoretical concept of single-cell configurations of rotating stall.
AB - The correlation between the frequencies of pressure oscillation ωosc and the rotor speed (frequencies of rotor rotation ωRR) under established rotating stall were determined by three methods: directly from the time diagram of the oscillation process, from the behavior diagram of parameters in space and time and from frequency characteristics. In total accordance with the Theory of Nonlinear Oscillation, by all methods of analysis, the links are in the form of integer ratios: ωosc / ωRR = 1:2 (for n/ nd= 0.6, where n - rotor speed in the experiment and nd- rotor speed from data-sheet) and ωosc / ωRR = 3:7 (for n/ nd = 0.8 and 0.95). The phases of parameter oscillations in the transverse cross-section are equal to the sensor angles in compressor stator. This is in agreement with the theoretical concept of single-cell configurations of rotating stall.
KW - Pressure oscillation
KW - Rotating stall
KW - Rotor speed
UR - http://www.scopus.com/inward/record.url?scp=0036919021&partnerID=8YFLogxK
U2 - 10.1515/TJJ.2002.19.4.233
DO - 10.1515/TJJ.2002.19.4.233
M3 - Article
AN - SCOPUS:0036919021
VL - 19
SP - 233
EP - 247
JO - International Journal of Turbo and Jet Engines
JF - International Journal of Turbo and Jet Engines
SN - 0334-0082
IS - 4
T2 - Tagung: Turbokompressoren im industriellen Einsatz
Y2 - 18 September 2002 through 19 September 2002
ER -