RAE2822 airfoil

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Revision as of 08:48, 16 September 2005 (view source) Praveen (Talk | contribs) ← Older edit		Revision as of 09:08, 16 September 2005 (view source) Praveen (Talk | contribs) Newer edit →
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-	[[Image:Rae2822.png]]	+	The freestream conditions are:
		+
		+	* Mach number = 0.729
		+	* Angle of attack = 2.31 deg.
		+	* Reynolds number = 6.5 million
		+
		+	[[Image:Rae2822.png | RAE2822 airfoil]]
		+
		+	== Results ==
		+
		+	[[Image:Vtc_rae2822_pressure.png | Pressure contours]]
		+
		+	[[Image:Vtc_rae2822_mach.png | Mach number contours]]

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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

Results