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RAE2822 airfoil

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[[Image:Rae2822.png]]
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The freestream conditions are:
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* Mach number = 0.729
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* Angle of attack = 2.31 deg.
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* Reynolds number = 6.5 million
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[[Image:Rae2822.png | RAE2822 airfoil]]
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== Results ==
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[[Image:Vtc_rae2822_pressure.png | Pressure contours]]
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[[Image:Vtc_rae2822_mach.png | Mach number contours]]

Revision as of 09:08, 16 September 2005

The freestream conditions are:

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

RAE2822 airfoil

Results

Pressure contours

Mach number contours

My wiki