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Automatic Plotting Routines for Estimating Static Aerodynamic Properties of Flared Projectiles for 2

机译:用于估算扩张弹丸静态空气动力学性质的自动绘图程序2

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This present report is intended to be used in the formulation of quick estimates of the static aerodynamic characteristics of the conventional flared projectile. The data is based primarily on References 2 (E.D. Boyer, 'Free Flight Range Tests of a Minuteman Re-entry Stage Model') and 5 (AMCP 706-280, 'Design of Aerodynamically Stabilized Free Rockets'), and the exposition follows that of the corresponding finned projectile presentation. The drag, static moment and normal force coefficients are determined from the simplified geometry of the projectile and the bounding aerodynamic conditions, i.e., sea level, flat fire, 2

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