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