User contributions for Daveg

23 May 2008

• 08:4108:41, 23 May 2008 diff hist +3,911‎ N Abstr:Flow over surface-mounted cube/rectangular obstacles ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-14=== ====Abstract==== Fluid flow past bluff obstacles - i.e. those whose geometry ensures that at all practical Reynolds numbers flow...
• 08:4008:40, 23 May 2008 diff hist +995‎ N Abstr:Flow over an isolated hill (without dispersion) ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-13=== ====Abstract==== The flow separation behind a smooth hill is the logical extension to the most widespread and basic CFD test cas...
• 08:3908:39, 23 May 2008 diff hist +36‎ Abstr:Stagnation point flow ‎No edit summary
• 08:3808:38, 23 May 2008 diff hist −14‎ Abstr:Stagnation point flow ‎No edit summary
• 08:3708:37, 23 May 2008 diff hist +5,053‎ N Abstr:Stagnation point flow ‎ New page: Semi-Confined Flows Underlying Flow Regime 3-12 Abstract The underlying flow regime (UFR) considered is the flow in a stagnation point. This type of flow regime is of considerable techn...
• 08:3208:32, 23 May 2008 diff hist +3,369‎ N Abstr:Pipe expansion (with heat transfer) ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-11=== ====Abstract==== The underlying flow regime (UFR) documented here, flow and heat transfer in a pipe expansion, relates to a flow...
• 08:2708:27, 23 May 2008 diff hist +3,591‎ N Abstr:The plane wall jet ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-10=== ====Abstract==== The underlying flow regime (UFR) – the plane wall jet - documented here is of major importance in many engine...
• 08:2608:26, 23 May 2008 diff hist 0‎ N File:UFR3-10.gif ‎No edit summary current
• 08:2408:24, 23 May 2008 diff hist 0‎ Abstr:Impinging jet ‎No edit summary
• 08:2408:24, 23 May 2008 diff hist +2,057‎ N Abstr:Impinging jet ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-09=== ====Abstract==== centre|thumb|465px|'''Figure 1.''' Schematic view of the flow. The flow under considerat...
• 08:2308:23, 23 May 2008 diff hist 0‎ N File:UFR3-09.jpg ‎No edit summary current
• 08:2008:20, 23 May 2008 diff hist 0‎ Abstr:3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation ‎No edit summary
• 08:1908:19, 23 May 2008 diff hist +72‎ Abstr:3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation ‎No edit summary
• 08:1808:18, 23 May 2008 diff hist +1,144‎ N Abstr:3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-08=== ====Abstract==== Boundary layers subject to an adverse pressure gradient are very often encountered in flows around bodies, and ...
• 08:1708:17, 23 May 2008 diff hist +1,368‎ N Abstr:Natural and mixed convection boundary layers on vertical heated walls (B) ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-07=== ====Abstract==== The effects of buoyancy on heat transfer can be predicted readily for laminar flows. When the flow is in the up...
• 08:1708:17, 23 May 2008 diff hist +1,205‎ N Abstr:Natural and mixed convection boundary layers on vertical heated walls (A) ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-06=== ====Abstract==== The flow under consideration is a low mach number flow of a strongly heated gas inside a vertical circular tube...
• 08:1608:16, 23 May 2008 diff hist +7,079‎ N Abstr:Shock/boundary-layer interaction (on airplanes) ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-05=== ====Abstract==== The interaction of a shock with a boundary layer developing on an aircraft wing can have an enormous impact on ...
• 08:1508:15, 23 May 2008 diff hist +7,217‎ N Abstr:Laminar-turbulent boundary layer transition ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-04=== ====Abstract==== Laminar-turbulent transition in boundary layers influences performance of many technical devices. The location ...
• 08:1408:14, 23 May 2008 diff hist +6,830‎ N Abstr:2D Boundary layers with pressure gradients (A) ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-03=== ====Abstract==== The underlying flow regime (UFR) – 2D Adverse Pressure Gradient Flows - documented here is of major importanc...
• 08:1308:13, 23 May 2008 diff hist 0‎ N File:UFR3-03.jpg ‎No edit summary current
• 08:1208:12, 23 May 2008 diff hist +5,347‎ N Abstr:Boundary layer interacting with wakes under adverse pressure gradient - NLR 7301 high lift configuration ‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-01=== ====Abstract==== The design of high-lift systems is an important issue in the aircraft industry, since it has a large impact on ...
• 08:1108:11, 23 May 2008 diff hist 0‎ Semi-confined Flows ‎No edit summary
• 08:1008:10, 23 May 2008 diff hist +3‎ Semi-confined Flows ‎No edit summary
• 08:1008:10, 23 May 2008 diff hist +41‎ Semi-confined Flows ‎No edit summary
• 08:0908:09, 23 May 2008 diff hist +1,595‎ N Semi-confined Flows ‎ New page: {| border="1" ! AC !! Application Challenges !! Contributor |- !3-01 | Boundary layer interacting with wakes under adverse pressure gradient - NLR 7301 high lift configuration || [[CF...
• 08:0208:02, 23 May 2008 diff hist +84‎ N ALSTOM Power (Switzerland) Ltd ‎ New page: ==Contributors== ===Dirk Wilhelm=== *Contributor of UFR2-07: 3D flow around blades current
• 08:0108:01, 23 May 2008 diff hist 0‎ University of Surrey ‎No edit summary current
• 08:0108:01, 23 May 2008 diff hist +11‎ University of Surrey ‎No edit summary
• 08:0108:01, 23 May 2008 diff hist +173‎ N University of Surrey ‎ New page: ==Contributors== ===Peter Voke=== *Contributor of UFR2-05: Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x106) *Reviewer of UFR2-09: Rotor/stator interaction
• 08:0008:00, 23 May 2008 diff hist +219‎ N Cranfield University ‎ New page: ==Contributors== ===Joanna Szmelter=== *Reviewer of AC1-04: Channel flow with wall injection *Contributor of UFR2-03: Flow around oscillating airfoil *Reviewer of UFR2-04: Flow around (... current
• 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