Home > Reports > Research reports > Implementation and futher application of refined transition prediction methods for turbomachinery and other aerodynamics flows. /Z - 1307/
Original title:
Implementation and futher application of refined transition prediction methods for turbomachinery and other aerodynamics flows. /Z - 1307/
Authors:
Jonáš, Pavel ; Příhoda, Jaromír Document type: Research reports
Year:
2001
Language:
eng Abstract:
The report deals with mathematical modelling and experimental investigation of the bypass transition in boundary-layer flows. The modelling of bypass transition is based on two-layer turbulence models and an algebraic intermittency model. The effect of velocity and length scales of free-stream turbulence on the onset and the end of the transition region for flat-plate boundary layer was investigated experimentally.
Keywords:
prediction methods; transition modelling; turbomachinery flows Project no.: GV101/98/K001 (CEP), GA101/00/1057 (CEP), IBS2076010 (CEP) Funding provider: GA ČR, GA ČR, GA AV ČR
Institution: Institute of Thermomechanics AS ČR
(web)
Document availability information: Fulltext is available at the institute of the Academy of Sciences. Original record: http://hdl.handle.net/11104/0107423