|
[Sponsors] |
![]() |
![]() |
#1 |
Member
Bineet Mehra
Join Date: Aug 2013
Posts: 61
Rep Power: 13 ![]() |
Attached is a figure showing the pressure coefficient distribution over the suction surface for two delta winglets(named surface 1 and surface 2) at a very high angle of attack of 45. The leading edge of the surface 2 is blunt(in the attached jpg).
Looking at the CP distribution, what obervations and conclusions can one make regarding the difference is separation, pressure drag and vortex structure of the two winglets ? |
|
![]() |
![]() |
![]() |
Tags |
pressure coefficients, separation bubble, vortex |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
static vs. total pressure | auf dem feld | FLUENT | 17 | February 26, 2016 13:04 |
Pressure coefficient | Giuseppe | FLUENT | 2 | July 26, 2015 03:19 |
error message | cuteapathy | CFX | 14 | March 20, 2012 06:45 |
lid-driven cavity in matlab using BiCGStab | Don456 | Main CFD Forum | 1 | January 19, 2012 15:00 |
Gas pressure question | Dan Moskal | Main CFD Forum | 0 | October 24, 2002 22:02 |