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Shock and Vibration
/
2021
/
Article
/
Fig 15
/
Research Article
Study on Flow Mechanism of a Morphing Supercritical Airfoil
Figure 15
Streamline over leeward flow field of the airfoil at the same camber (−3°) in one cycle (
M
= 0.74,
α
=
6
°
, and
f
= 1 Hz, CFD).
(a)
(b)