2021
DOI: 10.1007/978-981-15-7711-6_91
|View full text |Cite
|
Sign up to set email alerts
|

Performance Analysis of a Scramjet Combustor with Cavity for Mach Numbers 3.0, 3.25 and 3.50 with Hydrogen as a Fuel

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Year Published

2022
2022
2022
2022

Publication Types

Select...
4

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
references
References 18 publications
0
0
0
Order By: Relevance