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RAE2822 airfoil

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[[Image:Vtc_rae2822_mach.png | Mach number contours]]
[[Image:Vtc_rae2822_mach.png | Mach number contours]]
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[[Image:Vtc_rae2822_cp.png | Pressure coeffient]]

Revision as of 09:18, 16 September 2005

The freestream conditions are:

  • Mach number = 0.729
  • Angle of attack = 2.31 deg.
  • Reynolds number = 6.5 million

RAE2822 airfoil

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Pressure contours

Mach number contours


Pressure coeffient

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