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Shock and Vibration
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Shock and Vibration
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2021
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Article
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Tab 3
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Research Article
Study on Flow Mechanism of a Morphing Supercritical Airfoil
Table 3
Unsteady computational condition.
Flow condition
Mach number
Angles of attack (°)
Frequency reduction
CT1
0.6
2.89 + 2.41sin(w∗t)
0.0808