Hypersonic Propulsion
Hypersonic Propulsion is a form of aerospace propulsion technology that enables sustained vehicle flight at speeds exceeding Mach 5 by utilizing specialized propulsion systems designed to operate efficiently in the hypersonic flow regime.
2.1K
Publications
82.3K
Citations
4.1K
Authors
757
Institutions
Publications per year
2017–2026
478
2.1K
1–5 of 2.1K
4.1K
28
h-index
22
h-index
19
h-index
18
h-index
17
h-index
1–5 of 4.1K
757

Langley Research Center
Hampton, United States
47 h-index
435 publications
17.1K citations

National University of Defense Technology
Changsha, China
35 h-index
313 publications
13.4K citations

Harbin Institute of Technology
Harbin, China
33 h-index
322 publications
12K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
31 h-index
108 publications
6.9K citations

Ames Research Center
Mountain View, United States
27 h-index
111 publications
6.4K citations

Northwestern Polytechnical University
Xi'an, China
27 h-index
139 publications
5.8K citations

Beihang University
Beijing, China
27 h-index
166 publications
6.4K citations
University of Maryland, College Park
College Park, United States
26 h-index
99 publications
3.9K citations
1–8 of 757
250 publications · 11.9K citations
54
h-index
92 publications · 5K citations
41
h-index
AST · 137 publications · 4.9K citations
40
h-index
103 publications · 4K citations
35
h-index
90 publications · 3.5K citations
34
h-index
1–5