CFD Simulations of a Finned Projectile with Microflaps for Flow Control

Table 7

Variation of delta forces and moments due to microflaps with Mach, α = 0°.

Mach number	Delta normal force  (N)	Delta pitching moment  (N-m)	Delta axial force (N)
0.80	−10.9	1.23	3.7
0.90	−12.8	1.44	5.1
0.92	−12.8	1.44	5.4
0.95	−12.6	1.40	5.8
0.98	−11.8	1.30	6.3
1.1	−13.7	1.51	7.7
1.5	−34.4	4.13	13.1
2.0	−47.8	5.92	18.5
2.5	−60.6	7.56	23.7
3.0	−73.7	9.25	29.0
4.0	−103.9	13.05	43.1
5.0	−135.2	17.00	59.2