Laminar-turbulent transition prediction module for LOGOS package
A.V. Boiko1, Yu.M. Nechepurenko2, R.N. Zhuchkov3, and A.S. Kozelkov3
1 Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
2 Institute of Numerical Mathematics RAS, Moscow, Russia
3 Russian Federal Nuclear Center — All-Russian Research Institute of Experimental Physics, Sarov, Nizhny Novgorod Region, Russia
E-mail: boiko@itam.nsc.ru
Keywords: boundary layer, laminar-turbulent transition, linear stability theory, LOGOS
Abstract
The present work is devoted to a description and substantiation of an original module for computing the location of laminar-turbulent transition in subsonic boundary layer flows, which is based on the eN -method and enables more accurate computations of the flow around bodies in the presence of the so-called natural transition to turbulence in the boundary layer. A combined work of the module and the RANS solver from the aerodynamic part of the LOGOS package is demonstrated by the example of the flow past a flat plate. The obtained computed locations of the beginning and the end of the laminar-turbulent transition coincide with known reference values.
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