Imperial College London
Alternate

ProfessorRicardoMartinez-Botas

Faculty of Engineering, Department of Mechanical Engineering

Associate Dean Industry Partnerships,Prof of Turbomachinery
 
 
 
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Contact

 

+44 (0)20 7594 7241r.botas Website

 
 
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Location

 

611City and Guilds BuildingSouth Kensington Campus

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Summary

 

Publications

Citation

BibTex format

@article{Xue:2019:10.1016/j.ast.2019.105485,
author = {Xue, Y and Yang, M and Martinez-Botas, RF and Yang, B and Deng, K},
doi = {10.1016/j.ast.2019.105485},
journal = {Aerospace Science and Technology},
pages = {1--13},
title = {Unsteady performance of a mixed-flow turbine with nozzled twin-entry volute confronted by pulsating incoming flow},
url = {http://dx.doi.org/10.1016/j.ast.2019.105485},
volume = {95},
year = {2019}
}
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RIS format (EndNote, RefMan)

TY  - JOUR
AB  - Turbine with twin-entry volute has advantage of utilising energy from pulsatile exhaust gas and improving low-speed torque of an internal combustion engine. This paper investigates unsteady performance of a mixed flow turbine with nozzled twin-entry volute confronted by pulsatile incoming flow. The turbine performance at pulsating conditions with different Strouhal numbers (St) is studied via experimentally validated numerical method. Results show that the unsteadiness of turbine performance is enhanced as Strouhal number increases. In particular, the cycle-average efficiency at St = 0.522 is about 3.4% higher than that of quasi-steady condition (St = 0). Instantaneous loss breakdown of the turbine shows that the entropy generation rate of turbine components reduces evidently at pulsating conditions as Strouhal number increases, especially for the nozzle. Specifically, the cycle-averaged reduction of the loss in the nozzle is 37.3% at St = 0.522 compared with that of St = 0. The flow analysis shows that secondary flow which contributes to the majority of loss in the nozzle, including flow separation, horseshoe vortex, and reversed flow near the leading edge, are notably alleviated as Strouhal number increases. The alleviation of the flow structures are resulted from two reasons: one is that the flow distortion at the nozzle inlet is evidently depressed by the pulsating conditions, the other is that the inertia of the low momentum flow in the nozzle damps flow evolution at pulsating incoming flow. Consequently, the loss is reduced and the turbine performance is benefited by the pulsating inflows.
AU  - Xue,Y
AU  - Yang,M
AU  - Martinez-Botas,RF
AU  - Yang,B
AU  - Deng,K
DO  - 10.1016/j.ast.2019.105485
EP  - 13
PY  - 2019///
SN  - 1270-9638
SP  - 1
TI  - Unsteady performance of a mixed-flow turbine with nozzled twin-entry volute confronted by pulsating incoming flow
T2  - Aerospace Science and Technology
UR  - http://dx.doi.org/10.1016/j.ast.2019.105485
UR  - http://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:000503313200065&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=1ba7043ffcc86c417c072aa74d649202
UR  - https://www.sciencedirect.com/science/article/pii/S1270963819323430?via%3Dihub
UR  - http://hdl.handle.net/10044/1/76127
VL  - 95
ER  -
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