x - Aerospace Computing Lab - Stanford University
x - Aerospace Computing Lab - Stanford University
x - Aerospace Computing Lab - Stanford University
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Aerodynamic Sensitivities: FLO82<br />
RAE 2822 Airfoil<br />
α = 3.0 o , M∞ = 0.70<br />
Cp<br />
1.20 0.80 0.40 0.00 -0.40 -0.80 -1.20 -1.60 -2.00<br />
+<br />
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++ +++++++++++++++++++++++++<br />
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• 2D, cell-centered, finite volume Euler solver.<br />
• Multigrid.<br />
• Implicit residual smoothing.<br />
+<br />
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+<br />
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+ +++<br />
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+++ ++++++++++++++++++++++++<br />
• Artificial dissipation options: JST, CUSP, ECUSP<br />
and HCUSP.<br />
• Same numerical schemes as FLO87 and FLO107.<br />
– Joaquim Martins – January 12, 2000 – 14<br />
+ +++++ ++++++++++++++++++++++