What is it about?
Extremely high-speed flight can create dangerous oscillations of exposed skin panels, which can lead to failure and loss of the entire vehicle. Understanding changes in the behavior of the skin panels requires detailed parametric studies, which are provided in this paper.
Featured Image
Photo by Timothy Holmes on Unsplash
Why is it important?
This paper provides experimental results for a highly relevant but rarely investigated configuration. It further shows clear evidence of coupling between structure and flow using state-of-the-art full-field imaging techniques.
Perspectives
Featuring a significant portion of my PhD, this publication represents my structural dynamics perspective on this coupled multiphysics problem.
Marc Eitner
The University of Texas at Austin
Read the Original
This page is a summary of: Effect of Shock-Wave Boundary Layer Interaction on Vibratory Response of Compliant Panel, July 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2021-2493.
You can read the full text:
Resources
Contributors
The following have contributed to this page
