Semi-confined Flows: Difference between revisions

Revision as of 12:24, 3 March 2010

UFR	Underlying Flow Regime	Contributor	Organisation
3-01	Boundary layer interacting with wakes under adverse pressure gradient - NLR 7301 high lift configuration	Jan Vos	CFS Engineering SA
3-03	2D Boundary layers with pressure gradients (A)	Florian Menter	AEA Technology
3-04	Laminar-turbulent boundary layer transition	Andrzej Boguslawski	Technical University of Czestochowa
3-05	Shock/boundary-layer interaction (on airplanes)	Anthony Hutton	Qinetiq
3-06	Natural and mixed convection boundary layers on vertical heated walls (A)	André Latrobe	CEA / DRN / Department de Thermohydraulique
3-07	Natural and mixed convection boundary layers on vertical heated walls (B)	Mike Rabbitt	British Energy
3-08	3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation	Pietro Catalano	CIRA
3-09	Impinging jet	Jean-Paul Bonnet, Remi Manceau	Université de Poitiers
3-10	The plane wall jet	Jan Eriksson, Rolf Karlsson	Vattenfall Utveckling AB
3-11	Pipe expansion (with heat transfer)	Jeremy Noyce	Magnox Electric
3-12	Stagnation point flow	Beat Ribi	MAN Turbomaschinen AG Schweiz
3-13	Flow over an isolated hill (without dispersion)	Frederic Archambeau	EDF - R&D Division
3-14	Flow over surface-mounted cube/rectangular obstacles	Ian Castro	University of Southampton
3-15	2D flow over backward facing step	Arnau Duran	CIMNE
3-18	2D Boundary layers with pressure gradients (B)	Fred Mendonca	Computational Dynamics Ltd
3-30	2D Periodic Hill		Technische Universität München, Helmut-Schmidt Universität Hamburg

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