What is it about?

This paper investigates the influence of flow and acoustic uncertainties on the supersonic aircraft sonic boom. In order to reduce the computational cost and keep the prediction error low, we combine the outputs of low-fidelity and high-fidelity solvers using multi-fidelity analysis techniques.

Featured Image

Read the Original

This page is a summary of: Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction, Journal of Aircraft, December 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036962.
You can read the full text:

Read

Contributors

The following have contributed to this page