Normal Shock Relations
Normal Shock Relations is a theoretical framework in compressible flow that describes the conservation of mass, momentum, and energy across a one-dimensional, steady, adiabatic shock wave perpendicular to the flow direction, providing algebraic equations that relate flow properties upstream and downstream of the shock.
15
Publications
839
Citations
35
Authors
14
Institutions
Publications per year
2017–2026
2
Variants
Normal Shock Equations
Parents
15
Shock and Discontinuity Normals, Mach Numbers, and Related Parameters
S. J. Schwartz · 1998 · 165 citations
Drag coefficient of small spherical particles.
B. SELBERG, J. A. Nicholls · AIAA Journal · 1968 · 67 citations
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1 publications · 71 citations
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General Dynamics (United States)
Reston, United States
2 h-index
4 publications
64 citations

Hong Kong Polytechnic University
Hong Kong, Hong Kong
1 h-index
2 publications
36 citations
Institute of Mechanics
Beijing, China
1 h-index
3 publications
54 citations

Draper Laboratory
Cambridge, United States
1 h-index
1 publications
28 citations

Von Karman Institute for Fluid Dynamics
Sint-Genesius-Rode, Belgium
1 h-index
3 publications
39 citations

Chinese Academy of Sciences
Beijing, China
1 h-index
3 publications
54 citations

Ames Research Center
Mountain View, United States
1 h-index
1 publications
36 citations

Lund University
Lund, Sweden
1 h-index
1 publications
13 citations
1–8 of 14
2 publications · 84 citations
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Repository · 2 publications · 211 citations
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Repository · 1 publications · 36 citations
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Repository · 1 publications · 43 citations
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1 publications · 13 citations
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