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
/
2019
/
Article
/
Fig 5
/
Research Article
New Contour Design Method for Rocket Nozzle of Large Area Ratio
Figure 5
Comparison of the heat capacity ratio obtained with different assumptions.
