Model Coupling Mechanism for NASA Transonic Wind Tunnel

Model Coupling Mechanism for NASA Transonic Wind Tunnel

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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.

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