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Table 4 Results of radial expansion distance of debris cloud under different projectile density ratio
Fig.5 Pressure distribution in no tail-pipe SRM at different times
Fig.6 Gasflow velocity distribution in tail-pipe region of equilibrium state
Fig.6 Comparison of STG and PSOCG against highly maneuverable targets
Fig.7 Erosion process of projectile head at impact velocity of 4Ma
Fig.10 Stress of different materials with 4 mm thickness buffer layer charges
Fig.11 Stress of different materials with 4 mm thickness buffer layer charges
Fig.10 Time domain of the noise reduction algorithms
Fig.13 Aerodynamics and stability of three shapes
Fig.2 Axis wall pressure of combustor
Table 1 Main parameters of projectile material^[19-20]
Fig.3 Balance model after meshing
Fig.3 Command tracking of attitude response
Table 2 Main parameters of concrete materials^[22]
Fig.11 Frequency domain of the noise reduction algorithms
Fig.12 Time domain comparison of shock wave
Fig.13 Result of shock wave denoising
Fig.14 Result of shock wave denoising
Fig.10 Comparison of zero drift error curves before and after compensation^[46]
Fig.1 Principle of rotation modulation SINS

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