Zare Shahneh, Amir2018-02-282018-02-282015-04-30A. Zare Shahneh. Vortex generator effect on mitigation of separation in transonic flow nozzle. International Journal of Advancements in Mechanical and Aeronautical Engineering, 2015, Volume 2, Issue 1, pp61-652372-4153https://www.seekdl.org/journals-details.py/98?years=2015&volumes=62&issue=142https://dspace.lib.cranfield.ac.uk/handle/1826/13040The effect of tetrahedral sub-boundary layer vortex generator on plummeting normal shock-induced turbulent boundary layer separation has been investigated in computational environment and the result is presented. A good agreement achieved in this work between the pre-assessed experimental and current CFD results, opens the way for further utilization of CFD in the area of shock/boundary layer interaction with 3-D mean compressible flow field, particularly for complicated geometries. The outcome style sheet is illustrated by the portions given in this document.enCC0 1.0 Universalhttp://creativecommons.org/publicdomain/zero/1.0/separationnormal shock wavevortex generatorCFDSTAR-CDArticle