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23 May 2008
- 07:5807:58, 23 May 2008 diff hist −10 Flows Around Bodies No edit summary
22 May 2008
- 15:5815:58, 22 May 2008 diff hist +7,840 N Arch:Rotor/stator interaction New page: ==Flows Around Bodies== ===Underlying Flow Regime 2-09=== ====Abstract==== The underlying flow regime (UFR) rotor-stator interaction documented here is of major importance in many aerona...
- 15:5615:56, 22 May 2008 diff hist +2,373 N Abstr:3D flow around blades New page: ==Flows Around Bodies== ===Underlying Flow Regime 2-07=== ====Abstract==== The flow around turbomachinery blades is an important flow type for the power generation and aeropropulsion ind...
- 15:5515:55, 22 May 2008 diff hist +5,089 N Abstr:Flow around (airfoils and) blades (transonic) New page: ==Flows Around Bodies== ===Underlying Flow Regime 2-06=== ====Abstract==== The transonic flow through blade cascades is crucial problem for many turbomachinery applications. Blade cascad...
- 15:5315:53, 22 May 2008 diff hist +5,107 N Abstr:Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6) New page: ==Flows Around Bodies== ===Underlying Flow Regime 2-05=== ====Abstract==== The underlying flow regime of a standard single-element airfoil at the maximum lift condition documented here i...
- 15:5215:52, 22 May 2008 diff hist +11 Flows Around Bodies No edit summary
- 15:5015:50, 22 May 2008 diff hist −126 Abstr:Flow around (airfoils and) blades (subsonic) No edit summary
- 15:4315:43, 22 May 2008 diff hist +8,812 N Abstr:Flow around (airfoils and) blades (subsonic) New page: Flows Around Bodies Underlying Flow Regime 2-04 Abstract The Underlying Flow Regime entitled “Flow Around (Airfoils and) Blades” is of major importance in both the turbomachinery an...
- 15:3415:34, 22 May 2008 diff hist +2,960 N Abstr:Flow around oscillating airfoil New page: ==Flows Around Bodies== ===Underlying Flow Regime 2-03=== ====Abstract==== The flow around oscillating aerofoil is one of the fundamental and important problems investigated in aerospace...
- 15:3315:33, 22 May 2008 diff hist +3,730 N Abstr:Flow past cylinder New page: ==Flows Around Bodies== ===Underlying Flow Regime 2-02=== ====Abstract==== The flow past cylinders is an important flow type that occurs in many engineering applications. Although it was...
- 15:2615:26, 22 May 2008 diff hist +2,772 N Abstr:Flow behind a blunt trailing edge New page: ==Flows Around Bodies== ===Underlying Flow Regime 2-01=== ====Abstract==== The flow behind a blunt trailing edge is of interest to turbomachinery research due to its impact in the greate...
- 15:2515:25, 22 May 2008 diff hist 0 N File:URR2-01a.jpg No edit summary current
- 15:0615:06, 22 May 2008 diff hist 0 N File:UFR2-01.gif No edit summary current
- 13:0213:02, 22 May 2008 diff hist +789 N Flows Around Bodies New page: === State-of-the-Art Review === {| border="1" ! AC !! Application Challenges !! Contributor |- !2-01 | [[Flow behind a blunt trailing ed...
- 10:5310:53, 22 May 2008 diff hist −310 Free flows No edit summary
- 10:4910:49, 22 May 2008 diff hist +201 N ABB Alstom Power UK New page: ==Contributors== ===Peter Storey=== *Reviewer of AC6-03: Annular compressor cascade without clearance *Contributor of UFR1-05: Jet in a cross flow *Reviewer of UFR2-03: Flow around oscill... current
- 10:4810:48, 22 May 2008 diff hist +293 N Rolls Royce Deutschland New page: ==Contributors== ===Ruud Eggels=== *Reviewer of AC2-01: Bluff body burner for CH4-HE turbulent combustion *Reviewer of AC2-03: Gas burner controlled by variable density and/or counterflow... current
- 10:4710:47, 22 May 2008 diff hist +6 Abstr:Jet in a Cross Flow No edit summary
- 10:4410:44, 22 May 2008 diff hist −5 Abstr:Jet in a Cross Flow No edit summary
- 10:4410:44, 22 May 2008 diff hist +5 Abstr:Jet in a Cross Flow No edit summary
- 10:4310:43, 22 May 2008 diff hist +6,070 N Abstr:Jet in a Cross Flow New page: ==Free Flows== ===Underlying Flow Regime 1-05=== ====Abstract==== Understanding the underlying flow regime of a jet in cross flow documented here is basic to solving several problems of ...
- 10:4210:42, 22 May 2008 diff hist 0 N File:Image016.gif No edit summary
- 10:4010:40, 22 May 2008 diff hist 0 N File:UFR1-05 e.gif No edit summary current
- 10:3510:35, 22 May 2008 diff hist +88 Arch:Annular coaxial jets, flow and mixing No edit summary
- 10:3410:34, 22 May 2008 diff hist 0 Abstr:Underexpanded jet No edit summary
- 10:3210:32, 22 May 2008 diff hist +6 Abstr:Blade tip and tip clearance vortex flow No edit summary
- 10:3110:31, 22 May 2008 diff hist +42 Abstr:Blade tip and tip clearance vortex flow No edit summary
- 10:3010:30, 22 May 2008 diff hist 0 N File:UFR1-02.jpg No edit summary current
- 10:2910:29, 22 May 2008 diff hist +9,139 N Abstr:Blade tip and tip clearance vortex flow New page: ==Free Flows== ===Underlying Flow Regime 1-02=== ====Abstract==== The underlying flow regime (UFR) - wing/blade tip and tip clearance flow - documented here is of major importance in man...
- 10:2710:27, 22 May 2008 diff hist +105 Abstr:Underexpanded jet No edit summary
- 10:1610:16, 22 May 2008 diff hist +209,646 N Arch:State-of-the-Art Review: Turbomachinery Internal Flow New page: Introduction As part of the thematic network QNET-CFD, each thematic area co-ordinator has to produce an annual state-of–the-art review related to the application and validation of CFD ...
- 10:1510:15, 22 May 2008 diff hist +349 N Czech Academy of Sciences New page: ==Contributors== ===Jaromir Prihoda=== *Contributor of AC6-12: Steam turbine rotor cascade *Reviewer of AC6-06: Gas Turbine nozzle cascade *Contributor of UFR2-06: Flow around (airfoils ... current
- 10:1310:13, 22 May 2008 diff hist +284 N Sulzer Innotec AG New page: ==Contributors== ===Michael Casey=== *Contributor of AC6-08: High speed centrifugal compressor (In colaboration with Partner-28) *Reviewer of AC6-04: Pump turbine *Contributor of UFR1-0... current
- 10:1310:13, 22 May 2008 diff hist +218 N MAN Turbomaschinen AG Schweiz New page: ==Contributors== ===Beat Ribi=== * Contributor of AC6-08: High speed centrifugal compressor (In colaboration with Partner-09) * Contributor of UFR3-12: Stagnation point flow * Reviewer o... current
- 10:1210:12, 22 May 2008 diff hist +192 N Vattenfall Utveckling AB New page: ==Contributors== ===Jan Eriksson; Rolf Karlsson=== * Contributor of AC6-07: Draft tube * Contributor of UFR3-10: The plane wall jet * Reviewer of UFR3-11: Pipe expansion (with heat trans... current
- 10:1110:11, 22 May 2008 diff hist +297 N NTUA New page: ==Contributors== ===K. Papailiou=== * Contributor of AC6-05: Annular compressor cascade with tip clearance * Reviewer of AC6-12: Steam turbine rotor cascade * Contributor of UFR2-04: Fl... current
- 10:1010:10, 22 May 2008 diff hist +225 N AEA Technology New page: ==Contributors== ===Florian Menter=== * Contributor of AC6-04: Pump turbine * Reviewer of AC6-07: Draft tube * Contributor of UFR3-03: 2D Boundary layers with pressure gradients (A) * Re... current
- 10:1010:10, 22 May 2008 diff hist +243 N SNECMA Moteurs New page: ==Contributors== ===David Monet=== * Contributor of AC6-03: Annular compressor cascade without clearance * Reviewer of AC6-02: Low-speed centrifugal compressor * Reviewer of UFR4-07: D... current
- 10:0910:09, 22 May 2008 diff hist +255 N NUMECA International New page: ==Contributors== ===Nouredine Hakimi=== * Contributor of AC6-02: Low-speed centrifugal compressor * Reviewer of AC6-10: Axial compressor cascade * Contributor of UFR4-05: Curved passage ... current
- 10:0810:08, 22 May 2008 diff hist +2,221 N Abstr:Steam turbine rotor cascade New page: ==Application Area 6: Turbomachinery Internal Flows== ===Application Challenge AC6-12=== ====Abstract==== The results of experimental investigation of fluid flow in blade cascades at tra...
- 10:0610:06, 22 May 2008 diff hist +2,754 N Abstr:Axial compressor cascade New page: ==Application Area 6: Turbomachinery Internal Flows== ===Application Challenge AC6-10=== ====Abstract==== Experimental investigations on the boundary layer and loss behaviour on a high t...
- 10:0510:05, 22 May 2008 diff hist +5,647 N Abstr:High speed centrifugal compressor New page: ==Application Area 6: Turbomachinery Internal Flows== ===Application Challenge AC6-08=== ====Abstract==== The SRV2 is a high speed centrifugal impeller, with a very high total pressure r...
- 10:0410:04, 22 May 2008 diff hist +2,756 N Abstr:Draft tube New page: ==Application Area 6: Turbomachinery Internal Flows== ===Application Challenge AC6-07=== ====Abstract==== An experimental study has been performed of the flow in a sharp-heel draft tube ...
- 10:0310:03, 22 May 2008 diff hist 0 N File:AC6-07.gif No edit summary current
- 10:0110:01, 22 May 2008 diff hist +7,343 N Abstr:Gas Turbine nozzle cascade New page: ==Application Area 6: Turbomachinery Internal Flows== ===Application Challenge AC6-06=== ====Abstract==== The experimental cascade rig here suggested was investigated in the Von Karman I...
- 10:0010:00, 22 May 2008 diff hist +3,721 N Abstr:Annular compressor cascade with tip clearance New page: ==Application Area 6: Turbomachinery Internal Flows== ===Application Challenge AC6-05=== ====Abstract==== This application challenge deals with the flow prediction in the stationary annu...
- 09:5609:56, 22 May 2008 diff hist +3,634 N Arch:Pump turbine New page: ==Application Area 6: Turbomachinery Internal Flows== ===Application Challenge AC6-04=== ====Abstract==== The test case HV Pump-Turbine corresponds to a pump-turbine model designed and m...
- 09:4209:42, 22 May 2008 diff hist +3,334 N Arch:Annular compressor cascade without clearance New page: ==Application Area 6: Turbomachinery Internal Flows== ===Application Challenge AC6-03=== ====Abstract==== The NTUA test rig has been created to investigate the effects of tip clearance f...
- 09:4109:41, 22 May 2008 diff hist −6 Abstr:Low-speed centrifugal compressor No edit summary
- 09:4009:40, 22 May 2008 diff hist +12 Abstr:Low-speed centrifugal compressor No edit summary