Journals
Publish with us
Publishing partnerships
About us
Blog
Shock and Vibration
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
Shock and Vibration
/
2015
/
Article
/
Fig 7
/
Research Article
Impulse Force Balance for Ultrashort Duration Hypersonic Test Facilities
Figure 7
Typical system output obtained during shock tunnel testing. (a) Side force, (b) pitching, and (c) yawing components. AOA = 15°.
(a)
(b)
(c)