空气动力学
声学
压力传感器
网格
计算机科学
边界层
航空航天工程
流量(数学)
压力测量
电子工程
空气动力
传感器阵列
汽车工程
软件部署
工程类
互连
比例(比率)
机械工程
边界(拓扑)
材料科学
优化设计
边值问题
作者
Shizhen Yin,Yi Guo,Guannan Zheng,Juyao Li,Dilong Guo,Guowei Yang,Shuang Li,Liang Guo,Y W Su
摘要
ABSTRACT Accurate surface‐pressure mapping is crucial for aerodynamic optimization of high‐speed ground and air vehicles. However, existing air‐pressure‐sensing technologies cannot simultaneously achieve large‐area coverage, conformability to non‐developable surfaces, aerodynamic invisibility, and non‐invasiveness. Here, we present a stretchable, aerodynamic‐invisibility pressure‐sensor array that overcomes these limitations. This array integrates a 4 × 4 grid of miniaturized pressure sensors connected by stretchable multilayer serpentine interconnects that accommodate 30% strain, enabling conformal, non‐invasive deployment on complex surfaces. Owing to a non‐buckling interconnect design (thickness‐to‐width ratio of ∼0.55) that minimizes out‐of‐plane deformation, the array maintains a total thickness below ∼1.6 mm, remaining thin relative to the flow boundary layer and thus minimizing aerodynamic disturbance. Tests on a scale model of the Chinese standard electric multiple unit 3 (EMU‐3) in a moving train model system demonstrate accurate, spatially resolved surface‐pressure mapping consistent with numerical simulations, highlighting its great potential for aerodynamic testing and optimization in high‐speed vehicles.
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