A new method of quickly hypersonic waverider forebody configurations was developed.
发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法.
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A blended wing - body, variable camber wings, and forebody strakes provided extra lift and control.
翼身融合, 变曲率机翼, 还有前机身边条翼提供了额外的升力和控制性能.
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