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Model Coupling Mechanism for NASA Transonic Wind Tunnel · 模型 115468

作者：Luke Smallwood

From PDF description: The Primary design concept behind the Model Coupling Mechanism was to develop a reliable method of interchanging different test models within NASA’s wind tunnel. This design attempts to reduce time-consuming factors and human interaction within the wind tunnel’s test section, removing the need to wire up measurement systems and any lengthy installation processes, allowing tests to proceed at a much more efficient rate. Although this design focuses on a very specific section of the entire facility, the overall impact it could have for the future of wind tunnel tests would be substantial. Further details on this design are included with the attached PDF.

格式

STEP / IGES、Other、Rendering

分类

Aerospace、Industrial design、Machine design

标签

nasawindtunnelchallenge、space、tech、coupling、nasa、windtunnel、aerospace

数据更新

2026-07-12T00:59:15Z

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