Aerodynamic and angular motion characteristics of a fixed-canard dual-spin projectile under different forebody spinning ratesOA
Aerodynamic and angular motion characteristics of a fixed-canard dual-spin projectile under different forebody spinning rates
Wen JI;Chunlin GONG;Chunna LI;Gang WANG
School of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China||Shaanxi Aerospace Flight Vehicle Design Key Laboratory,Xi'an 710072,ChinaSchool of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China||Shaanxi Aerospace Flight Vehicle Design Key Laboratory,Xi'an 710072,ChinaSchool of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China||Shaanxi Aerospace Flight Vehicle Design Key Laboratory,Xi'an 710072,ChinaSchool of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China
Angular motionCoupled computational fluid dynamics and rigid body dynamicsDual-spin projectileNumerical simulationUnsteady aerodynamic characteristic
Angular motionCoupled computational fluid dynamics and rigid body dynamicsDual-spin projectileNumerical simulationUnsteady aerodynamic characteristic
《中国航空学报（英文版）》 2026 (8)
125-140,16
This research was supported by the National Natural Science Foundation of China(No.U2141254).
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