Erosive Burning
Erosive Burning is a phenomenon in solid rocket motor combustion characterized by increased propellant burn rate due to high-velocity crossflow of combustion gases, distinguishing it from quiescent or one-dimensional burning by incorporating aerodynamic shear effects that enhance heat transfer to the burning surface.
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2K
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117
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48
Institutions
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2017–2026
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Variants
Erosive Combustion
Parents
67
Erosive Burning of Some Composite Solid Propellants
León Green · Jet propulsion · 1954 · 74 citations
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Office National d'Études et de Recherches Aérospatiales, France
5 publications · 144 citations
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Office National d'Études et de Recherches Aérospatiales, France
4 publications · 87 citations
4
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Office National d'Études et de Recherches Aérospatiales, France
3 publications · 77 citations
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Pennsylvania State University
State College, United States
8 h-index
21 publications
858 citations
Office National d'Études et de Recherches Aérospatiales
Palaiseau, France
7 h-index
15 publications
424 citations
University of Illinois Urbana-Champaign
Urbana, United States
4 h-index
13 publications
535 citations
Princeton University
Princeton, United States
4 h-index
4 publications
101 citations
National Defense Academy of Japan
Yokosuka, Japan
2 h-index
4 publications
272 citations
Institute of Applied Mechanics
Moscow, Russia
2 h-index
2 publications
31 citations
Purdue University West Lafayette
West Lafayette, United States
2 h-index
4 publications
52 citations
Atlantic University
Virginia Beach, United States
2 h-index
2 publications
60 citations
1–8 of 48
17 publications · 437 citations
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10 publications · 427 citations
10
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6 publications · 129 citations
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3 publications · 120 citations
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3 publications · 71 citations
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