Search Results

User Name Remember Me Password

Showing results 1 to 6 of 6 Search took 0.00 seconds. Search: Posts Made By: Sudharshani

Forum: CFX October 13, 2009, 19:31

Replies: 22 convergent_divergent nozzle simulation in CFX-11 Views: 9,241 Posted By Sudharshani Inlet outlet BC, characteristic length hai....guys.... yes...i extended the nozzle additional area as a opening BC to cature the jet plume region. my questions are (1) how do u know ur Inlet velocity?..... did u get these figures like...

Forum: CFX October 9, 2009, 10:27

Replies: 22 convergent_divergent nozzle simulation in CFX-11 Views: 9,241 Posted By Sudharshani Hai... thanks for that...i will try that. in... Hai... thanks for that...i will try that. in the mean time i would like to see whats happening at the jet plume area of the nozzle exit( to c how the expansion +oblique shocks are being...

Forum: CFX October 9, 2009, 00:58

Replies: 22 convergent_divergent nozzle simulation in CFX-11 Views: 9,241 Posted By Sudharshani NPR Vs cross section area of supersonic nozzle hai..... i would like to know NPR (for supersonic nozzle is somewhere between 7:1 or 8:1) depends on the nozzle geometry( area ratio: exit/throat and inlet/throat)? sudharshani

Forum: CFX October 9, 2009, 00:47

Replies: 22 convergent_divergent nozzle simulation in CFX-11 Views: 9,241 Posted By Sudharshani supersonic CD nozzle hai..jwala R Thanks for that.....but CFX-Pre 11.0 i couldn't see Stagnation pressure as a icon under inlet condition. it had only two options : Static Pressure and Total pressure (stable) ...

Forum: CFX September 25, 2009, 03:31

Replies: 22 convergent_divergent nozzle simulation in CFX-11 Views: 9,241 Posted By Sudharshani mail ID sudharshani07@hotmail.com

Forum: CFX September 24, 2009, 09:43

Replies: 22 convergent_divergent nozzle simulation in CFX-11 Views: 9,241 Posted By Sudharshani B.C at the nozzle for simulation CFX 11.0 hai could u pls let know how did u set up the B.C at different conditions(from subsonic.sonic.supersonic and after that catching the expansion and oblique shock waves after exiting the divergent...

Showing results 1 to 6 of 6

Forum Jump User Control Panel Private Messages Subscriptions Who's Online Search Forums Forums Home General Forums     Main CFD Forum     System Analysis     Structural Mechanics     Electromagnetics     CFD Freelancers     Hardware     Lounge Software User Forums     ANSYS         CFX         FLUENT             Fluent Multiphase             Fluent UDF and Scheme Programming         ANSYS Meshing & Geometry     Autodesk Simulation CFD     AVL FIRE     COMSOL     CONVERGE     Fidelity CFD     FloEFD, FloWorks & FloTHERM     FLOW-3D     OpenFOAM         OpenFOAM News & Announcements             OpenFOAM Announcements from ESI-OpenCFD             OpenFOAM Announcements from OpenFOAM Foundation             OpenFOAM Announcements from Other Sources         OpenFOAM Installation         OpenFOAM Meshing & Mesh Conversion         OpenFOAM Pre-Processing         OpenFOAM Running, Solving & CFD         OpenFOAM Post-Processing         OpenFOAM Programming & Development         OpenFOAM Verification & Validation         OpenFOAM Community Contributions             OpenFOAM CC Toolkits for Fluid-Structure Interaction         OpenFOAM Journal         OpenFOAM Bugs     Phoenics     REEF3D         REEF3D News & Announcements     Siemens         STAR-CCM+         STAR-CD     SU2         SU2 News & Announcements         SU2 Installation         SU2 Shape Design Mesh Generation & Pre-Processing Software     ANSA     enGrid     GridPro     Pointwise & Gridgen Visualization & Post-Processing Software     EnSight     FieldView     ParaView     Tecplot Special Topics     Mesh Generation & Pre-Processing     Visualization & Post-Processing CFD Online Community     Site News & Announcements     Site Help, Feedback & Discussions     CFD-Wiki