Swiss/Finnish Collaboration on Aero-elastic Simulations for the F/A-18 Fighter
Vos, J. B.; Charbonnier, D.; Siikonen, T.; Salminen, E.; Gehri, A.; Stephani, P.
- Published
- Conference
- AIAA Aviation 2018, Atlanta, 2018. vol. AIAA-2018-3642.
CFSE editorial summary
This AIAA paper records a Swiss–Finnish collaboration on aeroelastic simulation of the F/A-18. CFSE’s public F/A-18 record describes the related dynamic study: tightly coupled CFD and structural solvers, a linear modal structural model, and vertical-tail buffeting as the problem used to generate aerodynamic component loads.
Practical takeaway
When using coupled simulations to assess aircraft loads, define the flight case, configuration, and structural model so each result stays tied to its modeled conditions.
Cite this paper
- Original paper DOI
- 10.2514/6.2018-3642
BibTeX citation
Select the citation text to copy it into your reference manager.
@inproceedings{vos2018_swiss_finnish_ae,
author = {Vos, J. B. and Charbonnier, D. and Siikonen, T. and Salminen, E. and Gehri, A. and Stephani, P.},
title = {Swiss/Finnish Collaboration on Aero-elastic Simulations for the F/A-18 Fighter},
booktitle = {AIAA Aviation},
address = {Atlanta},
year = {2018},
doi = {10.2514/6.2018-3642},
url = {https://doi.org/10.2514/6.2018-3642}
}Related services
- Fluid–structure interaction (FSI)
Structural integrity under fluid loading conditions.