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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2017
/
Article
/
Fig 9
/
Research Article
The Effect of Yaw Angle on a Compressible Rectangular Cavity Flow
Figure 9
Span-wise mean surface pressure distributions for
M
= 0.83: (a)
β
= 10° and (b)
β
= 45°.
(a)
β
= 10°
(b)
β
= 45°