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Published April 27, 2023 | Version v1
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MONNALISA_NUM_DA_0_SA_30_AR_5_TR_0.4_Delta_-20

Authors/Creators

  • 1. Politecnico di Milano
  • 2. Inria Centre de Recherche Saclay Île-de-France
  • 3. Airbus

Description

Upload of the numerical solutions for the Reference plane of the MONNALISA Project. Please, refer to the README file of this folder and to the articles associated.

Files

Files (21.9 GB)

Name Size
md5:66f4be90457dd22abbe814eb53819eda
21.9 GB Download

Additional details

Funding

European Commission
MONNALISA - Modelling Nonlinear Aerodynamics of Lifting Surfaces 101008257

References

  • Rausa, A., Gori, G., Guardone, A., Zanotti, A., & Auteri, F. (2022). Multi-fidelity assessment of the aerodynamic performances of unconventional aircraft tail configurations. In AIAA Aviation 2022 Forum (p. 3902).
  • Auteri, F., Gibertini, G., Gori, G., Guardone, A., Rausa, A., Zanotti, A., ... & Llamas-Sandin, R. C. (2022). MONNALISA: Modelling nonlinear aerodynamics of lifting surfaces. In AIAA Aviation 2022 Forum (p. 4149)
  • Zanotti, A., Rausa, A., Grassi, D., Riccobene, L., Gibertini, G., Guardone, A., & Auteri, F. (2022, June). Infrared Thermography Measurements over a Tail-Plane Model of a Large Passenger Aircraft. In Journal of Physics: Conference Series (Vol. 2293, No. 1, p. 012014). IOP Publishing.
  • Gori, G., Davoli, T. Rausa, A., Zanotti, A., Guardone, A. (2023). Bayesan calibration of a low order aerodynamic model for the design of unconventional tail empennages. In AIAA Aviation 2023 Forum (p.4422). Jun2 2023