Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration

<div>Tsai-Wu failure coefficient of the composite-reinforced wall panels. (a) Impact point A. (b) Impact point B (c). Impact point C.</div>

International Journal of Aerospace Engineering

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Figure 14

Figure 14: Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration 

Figure 14 | Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration 