Transonic Shock Waves is a fluid dynamic phenomenon characterized by the formation of shock waves in a flow field where the local Mach number transitions from subsonic to supersonic and back to subsonic within a localized region, typically occurring near solid boundaries at freestream Mach numbers close to unity.
321
Publications
13.4K
Citations
592
Authors
235
Institutions
Publications per year
2017–2026
45
Parents
Publications
321
Mathematical Aspects of Subsonic and Transonic Gas Dynamics
L. Howarth · Physics Bulletin · 1959 · 303 citations
Karl G. Guderley, E. V. Laitone · Journal of Applied Mechanics · 1963 · 194 citations · Full text
1–5 of 321
Authors
592
- HY
13
h-index
- ZX
11
h-index
- HY
10
h-index
- GC
8
h-index
- BL
7
h-index
1–5 of 592
Institutions
235
Nanjing University
Nanjing, China
12 h-index
19 publications
968 citations
Ames Research Center
Mountain View, United States
12 h-index
15 publications
507 citations
University of Michigan
Ann Arbor, United States
10 h-index
19 publications
532 citations
Fudan University
Shanghai, China
9 h-index
11 publications
573 citations
Princeton University
Princeton, United States
8 h-index
14 publications
751 citations
Langley Research Center
Hampton, United States
8 h-index
8 publications
358 citations
Chinese University of Hong Kong
Hong Kong, Hong Kong
7 h-index
12 publications
750 citations
University of Cambridge
Cambridge, United Kingdom
7 h-index
12 publications
422 citations
1–8 of 235
Venues
- AIAA Journal
46 publications · 2.2K citations
31
h-index
- Journal of Fluid Mechanics
15 publications · 878 citations
14
h-index
- Journal of Turbomachinery
11 publications · 356 citations
11
h-index
- Communications on Pure and Applied Mathematics
10 publications · 684 citations
10
h-index
- Journal of Differential Equations
9 publications · 261 citations
9
h-index
1–5