Research Article
CFD Simulations of a Finned Projectile with Microflaps for Flow Control
Table 8
Delta forces and moments due to microflaps, no fins, α= 0°.
| Mach number | Delta normal force (N) | Delta pitching moment (N-m) | Delta axial force (N) |
| 0.80 | –2.19 | 0.23 | 1.5 | 0.90 | –2.74 | 0.30 | 2.4 | 0.92 | –2.90 | 0.31 | 2.6 | 0.95 | –2.94 | 0.32 | 3.0 | 0.98 | –2.74 | 0.30 | 3.6 | 1.1 | –2.89 | 0.33 | 4.7 | 1.5 | –9.11 | 1.14 | 8.5 | 2.0 | –16.53 | 2.12 | 14.1 | 2.5 | –24.32 | 3.13 | 19.9 | 3.0 | –32.53 | 4.20 | 23.7 | 4.0 | –50.92 | 6.56 | 37.9 | 5.0 | –71.27 | 9.18 | 52.8 |
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