Journals
Publish with us
Publishing partnerships
About us
Blog
International Journal of Aerospace Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
International Journal of Aerospace Engineering
/
2012
/
Article
/
Fig 6
/
Research Article
Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner
Figure 6
HTPB baseline: ensemble average, experimental data
𝑟
𝑓
(
𝐺
o
x
)
and power law approximation, highlighting the diverging trends for
𝐺
o
x
>
100 kg/m
2
s.