UNSTEADY SHOCK WAVE – TURBULENT BOUNDARY LAYER INTERACTION IN THE LAVAL NOZZLE

The flow in transonic diffusers and supersonic air intakes often becomes unsteady due to shock wave-boundary layer interaction. Oscillations may be induced by natural separation unsteadiness or forced by boundary conditions. Significant improvements of CFD tools, increased computer resources and th...

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Bibliographic Details

Published in:	TASK Quarterly
Main Authors:	PIOTR DOERFFER, OSKAR SZULC, FRANCO MAGAGNATO
Format:	Article
Language:	English
Published:	Gdańsk University of Technology 2005-01-01
Subjects:	unsteady transonic flow shock wave nozzle flow
Online Access:	https://journal.mostwiedzy.pl/TASKQuarterly/article/view/2150