期刊
INTERNATIONAL JOURNAL OF TURBOMACHINERY PROPULSION AND POWER
卷 2, 期 2, 页码 -出版社
MDPI
DOI: 10.3390/ijtpp2020004
关键词
turbomachinery flows; transition models; boundary layers; bypass transition; separation-induced transition; wake-induced transition; Reynolds-averaged Navier-Stokes; intermittency; laminar kinetic energy
资金
- National Centre for Research and Development
- Avio Polska within the Innolot Coopernik project [INNOLOT/I/11/NCBR/2014]
Current models for transition in turbomachinery boundary layer flows are reviewed. The basic physical mechanisms of transition processes and the way these processes are expressed by model ingredients are discussed. The fundamentals of models are described as far as possible, with a common structure of the equations and with emphasis on the similarities between the models. Tests of models reported in the literature are summarized and our own test is added. A conclusion on the performance of models is formulated.
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