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Global stability of compressible flow about a swept parabolic body

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Figure 1.2. Sketch of viscous flow in the leading-edge region of a swept blunt body of infinite span (adapted from Poll, 1978).
Figure 1.3. Results from wind-tunnel experiments on a swept wing configuration with a semi-circular leading edge for a sweep angle Λ = 63 ◦
Figure 1.4. Sketch indicating the relevant instability mechanisms and the resulting transition regions on a swept wing depending on the sweep angle Λ (adapted from Oertel, Jr
Figure 1.5. Roadmap to transition as suggested by Morkovin et al. (1994) (see Reshotko, 1994).
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