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Figures

**Figure 1:** Flow around generic wing-body configuration - streamlines and pressure coefficient in three selected wing sections $\eta =\frac {X}{L}$ .
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**Figure 2:** Flow around Onera A airfoil ( $Re=2\cdot 10^6$ , , $\alpha =13.3^o$ ) velocity and shear-stress profiles on the suction side.
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**Figure 3:** Transonic flow around RAE-2822 airfoil (Case 9, left: $Re=6.5 \; 10^6$ , ; Case 10, left: $Re=6.2 \; 10^6$ , , $\alpha =2.79^o$ ) - distribution of pressure coefficient.
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Markus Schatz 2004-02-10