What deserves special mention is that a distinct difference exists between the design technology of the fairing on a carrier rocket and that of a multiple-warhead missile.
更需要指出的是,运载火箭整流罩的设计技术与导弹多弹头整流罩设计技术存在显著的不同。
Below is a top-down view of an airflow analysis of the same design on an A320, with the associated pressure contours for an unmodified and modified fairing.
以下是A320气动性能分析的俯视图。图5 a显示的是未经改装的整流罩上的压力分布图。
Ben designed the fairing shell to have a drag coefficient that would allow me to achieve at least 50 KPH on less than 130 watts of power.
本设计的整流罩外壳有阻力系数,使我实现至少50公里不到13 0瓦的功率。
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