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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The work was financially supported by the Federal State Unitary Enterprise “RFYaTs-VNIIEF” (Contract No. 13058-12) and by the Russian Foundation for Basic Research (Projects Nos. 13-01-00270 and 13-01-00350).
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Boiko, A.V., Nechepurenko, Y.M., Zhuchkov, R.N. et al. Laminar-turbulent transition prediction module for LOGOS package. Thermophys. Aeromech. 21, 191–210 (2014). https://doi.org/10.1134/S0869864314020061
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DOI: https://doi.org/10.1134/S0869864314020061