RAE2822 airfoil
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(Difference between revisions)
| Line 9: | Line 9: | ||
== Results == | == Results == | ||
| + | ===Pressure contours=== | ||
[[Image:Vtc_rae2822_pressure.png | Pressure contours]] | [[Image:Vtc_rae2822_pressure.png | Pressure contours]] | ||
| - | [[Image:Vtc_rae2822_mach.png | Mach number contours]] | + | ===Mach number contours=== |
| + | [[Image:Vtc_rae2822_mach.png | Mach number contours | center]] | ||
| - | [[Image:Vtc_rae2822_cp.png | Pressure coeffient]] | + | |
| + | [[Image:Vtc_rae2822_cp.png | Pressure coeffient | center | 550px]] | ||
Revision as of 09:28, 16 September 2005
The freestream conditions are:
- Mach number = 0.729
- Angle of attack = 2.31 deg.
- Reynolds number = 6.5 million
Results
Pressure contours
Mach number contours
