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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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Tab 3
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Research Article
CFD Simulations of a Finned Projectile with Microflaps for Flow Control
Table 3
New geometric parameters used for 2-microflap configurations (case
).
Case
Axial spacing (m)
Circumferential spacing in angles (°)
Case
: 6 flaps
0.0079, 0.0079, 0.0079
20, 40, 60
Case
: 6 flaps
0.006, 0.01, 0.01349
20, 40, 60
Case
: 8 flaps
0.006, 0.006, 0.006, 0.006
20, 35, 50, 65
Case
: 8 flaps
0.006, 0.008, 0.008, 0.00749
20, 35, 50, 65