Semi-confined Flows: Difference between revisions

Revision as of 11:32, 7 April 2009

UFR	Underlying Flow Regime	Contributor
3-01	Boundary layer interacting with wakes under adverse pressure gradient - NLR 7301 high lift configuration	CFS Engineering SA
3-03	2D Boundary layers with pressure gradients (A)	AEA Technology
3-04	Laminar-turbulent boundary layer transition	Technical University of Czestochowa
3-05	Shock/boundary-layer interaction (on airplanes)	Qinetiq
3-06	Natural and mixed convection boundary layers on vertical heated walls (A)	CEA / DRN / Department de Thermohydraulique
3-07	Natural and mixed convection boundary layers on vertical heated walls (B)	British Energy
3-08	3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation	CIRA
3-09	Impinging jet	Université de Poitiers
3-10	The plane wall jet	Vattenfall Utveckling AB
3-11	Pipe expansion (with heat transfer)	Magnox Electric
3-12	Stagnation point flow	MAN Turbomaschinen AG Schweiz
3-13	Flow over an isolated hill (without dispersion)	EDF - R&D Division
3-14	Flow over surface-mounted cube/rectangular obstacles	University of Southampton
3-15	2D flow over backward facing step	CIMNE
3-18	2D Boundary layers with pressure gradients (B)	Computational Dynamics Ltd
3-19	Bypass transition on a flat plate	Fachhochschule Niederrhein

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-| [[Pipe expansion (with heat transfer)]] || [[Magnox Electric]]
+| [[Pipe expansion (with heat transfer)]] [[Image:Star_red.jpg]]|| [[Magnox Electric]]
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-| [[Flow over surface-mounted cube/rectangular obstacles]] || [[University of Southampton]]
+| [[Flow over surface-mounted cube/rectangular obstacles]] [[Image:Star_red.jpg]]|| [[University of Southampton]]
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