Impact of leakage inlet swirl angle in a rotor-stator cavity on flow pattern, radial pressure distribution and frictional torque in a wide circumferential reynolds number range
In: 13th European Turbomachinery Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2019 - ETC 2019; Lausanne; Switzerland; 8 - 12 April 2019 - European Turbomachinery Society, 2019
2019book article/chapter in Proceedings
Mechanical EngineeringFaculty of Engineering » Maschinenbau und Verfahrenstechnik » Institute for Energy and Materials Processes (EMPI)Faculty of Engineering » Maschinenbau und Verfahrenstechnik » Institut für Energie- und Umweltverfahrenstechnik » Turbomachinery
Title in English:
Impact of leakage inlet swirl angle in a rotor-stator cavity on flow pattern, radial pressure distribution and frictional torque in a wide circumferential reynolds number range
Author:
Schröder, Tilman RaphaelUDE
- LSF ID
- 58383
- ORCID
- 0000-0002-2625-7846
- Other
- connected with university
- GND
- 1208807471
- LSF ID
- 1605
- ORCID
- 0000-0003-0828-2324
- Other
- connected with university
- GND
- 1144405912
- LSF ID
- 55986
- ORCID
- 0000-0002-5025-9163
- Other
- connected with university
- GND
- 1081949767
- LSF ID
- 1008
- ORCID
- 0000-0002-6760-9940
- Other
- connected with university
Scopus ID
Language of text:
English
Keyword, Topic:
Centripetal through-flow ; Leakage flow ; Rotor-stator cavity ; Axial thrust ; Centripetal through-flow ; Disc torque ; Leakage flow ; Radial pressure distribution ; Rotor-stator cavity