UFR Index

Flow Type	UFR	Underlying Flow Regime	Contributor
Free Flows	1-01	Underexpanded jet	Health and Safety Laboratory
	1-02	Blade tip and tip clearance vortex flow	Sulzer Innotec AG
	1-05	Jet in a Cross Flow	ABB Alstom Power UK
	1-06	UFR_1-06	Lea Associates
Flows around Bodies	2-01	Flow behind a blunt trailing edge	Vrije Universiteit Brussel
	2-02	Flow past cylinder	Universität Karlsruhe
	2-03	Flow around oscillating airfoil	Cranfield University
	2-04	Flow around (airfoils and) blades (subsonic)	NTUA
	2-05	Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6)	University of Surrey
	2-06	Flow around (airfoils and) blades (transonic)	Czech Academy of Sciences
	2-07	3D flow around blades	ALSTOM Power (Switzerland) Ltd
Semi-confined Flows	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