AIAA Aviation 2019 Forum 2019
DOI: 10.2514/6.2019-3630
|View full text |Cite
|
Sign up to set email alerts
|

Comparison of Computational and Experimental Results in the Wake Region Behind a Wall-Mounted Hemisphere in Supersonic Flow

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Year Published

2021
2021
2021
2021

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
references
References 12 publications
0
0
0
Order By: Relevance