Combustion: Difference between revisions
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=== [[State-of-the-Art Review]] === | |||
{| border="1" | |||
! AC !! Application Challenges !! Contributor | |||
|- | |||
! 1-01 | |||
| [[Aero-acoustic cavity]] || [[Computational Dynamics Ltd]] | |||
|- | |||
! 1-02 | |||
| [[RAE M2155 Wing]] || [[CIRA]], [[Qinetiq]] | |||
|- | |||
! 1-04 | |||
| [[Channel flow with wall injection]] || [[SNPE Propulsion]] | |||
|- | |||
! 1-05 | |||
| [[Ahmed body]] || [[Université de Poitiers]] | |||
|- | |||
! 1-08 | |||
| [[L1T2 3 element airfoil]] | |||
| [[CFS Engineering SA]], [[Qinetiq]] | |||
|} | |||
Revision as of 13:28, 20 May 2008
State-of-the-Art Review
| AC | Application Challenges | Contributor |
|---|---|---|
| 1-01 | Aero-acoustic cavity | Computational Dynamics Ltd |
| 1-02 | RAE M2155 Wing | CIRA, Qinetiq |
| 1-04 | Channel flow with wall injection | SNPE Propulsion |
| 1-05 | Ahmed body | Université de Poitiers |
| 1-08 | L1T2 3 element airfoil | CFS Engineering SA, Qinetiq |