The stability of rolling motion of hypersonic vehicles with slender configuration under pitching ma

• 作 者: YE YouDa TIAN Hao ZHANG XiaFen
• 机 构: StateKeyLaboratoryofAerodynamics,NationalLaboratoryforComputationalFluidDynamics
• 出 处: 中国科学：物理学、力学、天文学英文版
• 发表日期: 2015年6期
• 关键词: 高超音速飞行器 操纵稳定性 滚动运动 NAVIER-STOKES方程 配置 高超声速飞行器 稳定性分析 数值模拟 stability rolling moti
• 基金项目: This work was supported by the National Natural Science Foundation of China （Grant Nos. 91216203 and 91216304）. The first author appreciates CAS Academician ZHANG HanXin and CAS Academician ZHOU Heng

The configurations of near space hypersonic flying vehicles are considerably different from those of conventional aircrafts.Their configurations are relatively slender;hence their moment of inertia around the longitudinal axis is much smaller than those a