Accurate numerical simulation on the structural response of the VEGA payload fairing using modal coupling approach-Reference-Cited by-同舟云学术

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Accurate numerical simulation on the structural response of the VEGA payload fairing using modal coupling approach

Published:2018-11-24 Issue:2 Volume:11 Page:173-183
ISSN:1868-2502
Container-title:CEAS Space Journal
language:en
Short-container-title:CEAS Space J

Author:

Schmidt H.,Koh S.,Dafnis A.,Schröder K.-U.,Schröder W.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1007/s12567-018-0225-5.pdf

Reference18 articles.

1. Economon, Thomas D., et al.: SU2: an open-source suite for multiphysics simulation and design. AIAA J. 54(3), 828–846 (2016)

2. Beckert, A., Wendland, H.: Multivariate interpolation for fluid–structure-interaction problems using radial basis functions. Aerosp. Sci. Technol. 5, 125–134 (2001). (Art. No. 5125)

3. Neumann, J., Krüger, W.: Coupling Strategies for Large Industrial Models, Computational Flight Testing, vol. 123. Series Notes on Numerical Fluid Mechanics and Multidisciplinary Design. pp. 207–222 (2012)

4. Sanchez, R., et al.: Assessment of the fluid–structure interaction capabilities for aeronautical applications of the open-source solver SU2. In: VII European Congress on Computational Methods in Applied Sciences and Engineering (2016)

5. Capri, F., et al.: Linearized aeroelastic analysis for a launch vehicle in transonic flight conditions. J. Spacecr. Rockets 43(1), 92–104 (2006)

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1. Aerodynamic Heating Analysis on Rocket Fairings Using CFD and DSMC;Journal of the Korean Society of Propulsion Engineers;2024-08-31

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