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ED1: Design and Prototype of a 3D Printed Wind Tunnel Model with Integrated Force MeasurementWind tunnel testing using conventionally manufactured force measurement systems (balances) is able to yield precise and accurate results. These balances are delicate, complex instruments. Due to the nature of this high-precision complexity, balances are expensive and time-consuming to produce. These factors can limit the design potential of the model because using conventionally manufactured balances generally means that the model is designed to accommodate balances that already exist. Ideally, engineers would be able to design a measurement system that is tailored to fit the needs of the model, rather than the other way around. The goal of this research project was to determine if it is possible to overcome these drawbacks by designing a wind tunnel model with a modifiable integrated force measurement system that leverages additive manufacturing. This was undertaken by utilizing the existing UT-63 wind tunnel balance (measurement system), integrating it with a model based on the existing AGARD-B model, and performing stress analysis to optimize the design. Due to time constraints, the result of this endeavor is currently incomplete. Continued analysis and optimization are required to have a thorough understanding of the success or failure of the attempted design. As additive manufacturing technology evolves, the ability for it to become the primary method of fabrication for sensitive measurement systems increases. This project contributes to this by providing one method for design, a framework for optimizing existing balances for additive manufacturing, and resources for performing necessary stress analysis.
Document ID
20210020456
Acquisition Source
Langley Research Center
Document Type
Other - Technical report
Authors
Callie Ellsworth
(STEM Takes Flight)
Date Acquired
August 12, 2021
Publication Date
August 13, 2021
Subject Category
Aeronautics (General)
Funding Number(s)
CONTRACT_GRANT: 80NSSC20M0056
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
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