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Verification and Validation for a Finite Element Model of a Hyperloop Pod Space Frame

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Model Validation and Uncertainty Quantification, Volume 3

Abstract

This paper discusses the verification and validation of a finite element (FE) model of the space frame built by the Hyperloop University of Cincinnati (HUC) team for the first student design competition organized by SpaceX. For the purpose of studying the frame performance in various dynamic scenarios, development of a reliable FE model was crucial. A verification and validation (V&V) strategy utilizing physical modal tests and torsional stiffness tests was adopted to ensure that the FE model was capable of accurately capturing the dynamic characteristics of the constructed space frame. This work aims to present the details of the V&V activities as performed on the main frame.

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References

  1. Musk, E.: Hyperloop alpha. SpaceX, 2013

    Google Scholar 

  2. AIAA: Guide for the Verification and Validation of Computational Fluid Dynamics Simulations, AIAA G-077-1998, 1998

    Google Scholar 

  3. American Society of Mechanical Engineers (ASME): Guide for Verification and Validation in Computational Solid Mechanics, ASME V&V. American Society of Mechanical Engineers, New York (2006)

    Google Scholar 

  4. Friswell, M.I., Mottershead, J.E.: Finite Element Model Updating in Structural Dynamics. Kluwer Academic Publishers, Dordrecht (1995)

    Book  Google Scholar 

  5. Pasha, H.G., Kohli, K., Allemang, R.J., Phillips, A.W., Brown, D.L.: Structural dynamics model calibration and validation of a rectangular steel plate structure. In: Conference Proceedings of the Society for Experimental Mechanics Series, Vol. 3, pp. 351–362, 2015

    Google Scholar 

  6. Jayakumar, V., Kim, J.: A Two-Step Approach to Build a FEM Model of a Built-Up Structure with Special Attention to Description of Boundary Conditions and System Damping. INTER-NOISE and NOISE-CON Congress and Conference Proceedings, NoiseCon17, Grand Rapids, MI, pp. 1–1004, 786-797(12)

    Google Scholar 

  7. Chung, H.: Free vibration analysis of circular cylindrical shells. J. Sound Vib. 74(3), 331–350 (1981)

    Article  Google Scholar 

  8. Vold, H., Kundrat, J., Rocklin, T., Russell, R.: A multi-input modal estimation algorithm for mini-computers. SAE Transact. 91, 815–821 (1982)

    Google Scholar 

  9. Allemang, R.J., Brown, D.L.: A correlation coefficient for modal vector analysis. In: Proceedings, International Modal Analysis Conference. pp. 110–116 (1982)

    Google Scholar 

  10. Steed, Thomas. Torsional Stiffness Measuring Machine (TSMM) & Automated Frame Design Tools (Master’s Thesis), University of Cincinnati, 2009

    Google Scholar 

  11. Young, Alexander: Validating Automotive Frame Torsion Stiffness Measurement Techniques (Master’s Thesis), University of Cincinnati, 2016

    Google Scholar 

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Acknowledgement

The Hyperloop pod design venture was a massive team effort of over 50 student volunteers across Mechanical Engineering, Aerospace Engineering, Electrical Engineering and Computer Science departments as well as Lindner Business College and College of Design, Architecture and Art Planning of which the presented material forms a small component and could not have been completed without their contribution to the project. The authors would like to acknowledge the entire Hyperloop UC team for their efforts as a collective group in the design of the pod and accompanying test setups.

Hyperloop UC was fortunate to have sponsors who provided technical advice and manufacturing help particularly Justin Atkins (Cincinnati Incorporated), Tri-State Fabricators and Jack Malluege (ANSYS), their support is highly appreciated. The authors would also like to acknowledge the contributions of Ronald Hudepohl for his manufacturing guidance and Dr. Randall Allemang for his valuable technical guidance and for the use of SDRL lab space and resources for testing activities. Additionally, we would like to thank SpaceX for organizing this competition.

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Correspondence to Vignesh Jayakumar .

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© 2020 Society for Experimental Mechanics, Inc.

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Jayakumar, V. et al. (2020). Verification and Validation for a Finite Element Model of a Hyperloop Pod Space Frame. In: Barthorpe, R. (eds) Model Validation and Uncertainty Quantification, Volume 3. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-030-12075-7_4

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  • DOI: https://doi.org/10.1007/978-3-030-12075-7_4

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-12074-0

  • Online ISBN: 978-3-030-12075-7

  • eBook Packages: EngineeringEngineering (R0)

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