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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2017
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Article
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Fig 7
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Research Article
CFD Simulations of a Finned Projectile with Microflaps for Flow Control
Figure 7
Computed surface pressure contours in the afterbody fin region near the microflap for a 1-flap case,
= 2.5,
α
= 0°.