Journal of Projectiles, Rockets, Missiles and Guidance

Influence of Booster on Aerodynamic Characteristics and Stability of Cruise Missile

ZHANG Yang, JIANG Shengju, TONG Jing, SHI Yongbin, BU Yuepeng

JPRMG, 2024, 44(2): 51-56. DOI: 10.15892/j.cnki.djzdxb.2024.02.008

Fig.13 Aerodynamics and stability of three shapes

Other figure/table from this article

Fig.1 Appearance of cruise missile
Fig.2 Geometric dimensions of boattail(mm)
Fig.3 Booster appearance before and after separation
Fig.4 Mesh division
Fig.5 Comparison of aerodynamic characteristics and stability of booster before and after separation
Fig.6 Surface flow state of booster before and after separation at angle of attack is 0°
Fig.7 Surface flow state of booster before and after separation at angle of attack is 4°
Fig.8 Distribution of pressure at different sections of booster before and after separation
Fig.9 Sections position
Fig.10 Surface flow state of σ₁ shape
Fig.11 Surface flow state of σ₂ shape
Fig.12 Cross section pressure distribution at different σ
Fig.14 Surface flow state of original curve-smooth shape
Fig.15 Surface flow state of σ₂ curve-smooth shape
Fig.16 Distribution of pressure at different sections of different curve-smooth shape
Fig.17 Aerodynamics and stability of four shapes