Publication not explained

This publication has not yet been explained in plain language by the author(s). However, you can still read the publication.

If you are one of the authors, claim this publication so you can create a plain language summary to help more people find, understand and use it.

Featured Image

Read the Original

This page is a summary of: Uncertainty Quantification Based Receptivity Modelling of Crossflow Instabilities Induced by Distributed Surface Roughness in Swept Wing Boundary Layers, June 2013, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2013-3106.
You can read the full text:

Read

Contributors

The following have contributed to this page