Experimental Study into the Flow Physics of Three-Dimensional Shock Control

This interview describes a fundamental experimental study of the flow structure around a single three-dimensional (3-D) transonic shock control bump (SCB) mounted on a flat surface in a wind tunnel.

Image courtesy of interviewee

Leave a Reply

Your email address will not be published.

×
Guest visitors to the Faculti website can view any insight monthly. You have insight(s) remaining for this month

Register for free as an individual and view thousands of insights in our archive today or subscribe for subject access.

You may already have institutional access to Faculti. Please access Faculti using your institution credentials.

Copyright © Faculti Media Limited 2022. All rights reserved.
error:

Add the Faculti Web App to your Mobile or Desktop homescreen

Install
×