Research Article
CFD Simulations of a Finned Projectile with Microflaps for Flow Control
Table 6
Variation of delta forces and moments due to microflaps with angle of attack,
= 2.5.
| Angle of attack (°). | Delta normal force (N) | Delta pitching moment (N-m) | Delta axial force (N) |
| −16 | −100.0 | 13.19 | 49.1 | −12 | −91.7 | 11.96 | 43.9 | −8 | −91.7 | 11.91 | 39.7 | −4 | −81.6 | 10.49 | 33.7 | −2 | −72.0 | 9.19 | 28.7 | 0 | −61.6 | 7.74 | 23.4 | 2 | −52.5 | 6.48 | 19.2 | 4 | −45.7 | 5.56 | 16.7 | 8 | −44.5 | 5.29 | 16.0 | 12 | −57.4 | 6.85 | 18.3 | 16 | −64.0 | 7.51 | 19.2 |
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