Page 140 - 《爆炸与冲击》2026年第2期

第 46 卷 白春玉，等： 不同垂向速度下翼身融合民机机体的坠撞响应 第 2 期

(4) 翼身融合机体在坠撞响应中体现了一定的鲁棒性，其结构破坏模式、乘员伤害响应、结构吸能特
性在 7.92～9.14 m/s 工况下趋于一致。
研究成果能为 BWB 民机的适航要求制定和结构抗坠撞优化设计提供参考。但所采用的模型存在
一定的局限性，例如模型忽略了连接件、座椅系统在坠撞过程中的影响，后续将做进一步研究。

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