CFD Simulations of a Finned Projectile with Microflaps for Flow Control

Table 2

Delta forces and moments due to microflaps, = 2.5, = 0°.

Cases	Delta normal force  (N)	Delta pitching moment  (N-m)	Delta axial force (N)
4 flaps, [46]	–40.0	4.20	17.0
Case : 6 flaps	–47.5	5.87	19.9
Case : 6 flaps	–50.2	6.23	20.0
Case : 6 flaps	–50.8	6.34	21.2
Case : 8 flaps	–51.4	6.25	20.2
Case : 8 flaps	–52.5	6.34	21.6
Case : 8 flaps	–55.5	6.80	23.1
1-flap case	–11.0	1.50	6.0