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Quasi-equilibrium glide trajectory design of waverider-based hypersonic vehicle

机译:基于乘波体的高超音速飞行器的准平衡滑行轨迹设计

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the primary objective of this work is to carry out the 3D parametric geometry representations of hypersonic waveriders, and to calculate its aerodynamics by engineering experiential formula. Finally, an approach is proposed to determine a quasi-equilibrium glide trajectory with constraint on the stagnation point heat transfer rate. The benefit of solving this problem is that the angle of attack is the only control to be determined.
机译:这项工作的主要目的是对高超音速乘波器进行3D参数化几何表示,并通过工程经验公式来计算其空气动力学。最后,提出了一种确定驻点传热速率的准平衡滑行轨迹的方法。解决此问题的好处在于,迎角是唯一要确定的控制方式。

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