To introduce virtual certification tools and procedures into in-flight ice accretion and IPS certification
- Definition of metrics that can assess the quality of a simulation compared to reference (experimental) results
- Definition of methods to assess the validity of a simulation when limited or null direct experimental comparison exists. In this process, EASA will provide authority perspective on criteria that must be met
Design of an electro-thermal Ice Protection System (PWG3)
- Arizmendi, B., Morelli, M., Parma, G., Zocca, M., Quaranta, G., Guardone, A. (2021). In-flight Icing: Modeling, Prediction, and Uncertainty. In: Vasile, M. (eds) Optimization Under Uncertainty with Applications to Aerospace Engineering. Springer, Cham. https://doi.org/10.1007/978-3-030-60166-9_15
- “Preliminary Guidelines for the Rotorcraft Certification by Simulation Process,” 2022 www.rocs-project.org/guidelines/
- ASME, Standard for Verification and Validation in Computational Fluid Dynamics and Heat Transfer, New York, NY: The American Society of Mechanical Engineers, 2009
- Gori, G., Congedo, P. M., Le Maître, O., Bellosta, T., & Guardone, A. (2022). Modeling in-flight ice accretion under uncertain conditions. Journal of Aircraft, 59(3), 799-813. https://doi.org/10.2514/1.C036545
