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.

67

Publications

2K

Citations

117

Authors

48

Institutions

Publications per year

2017–2026

0

Variants

Erosive Combustion

Authors

117

  1. MK
    Merrill K. King

    Atlantic University, United States

    5 publications · 153 citations

    5

    h-index

  2. GL
    G. LENGELLE

    Office National d'Études et de Recherches Aérospatiales, France

    5 publications · 144 citations

    5

    h-index

  3. KK
    K. K. Kuo

    Pennsylvania State University, United States

    5 publications · 126 citations

    5

    h-index

  4. JC
    J. C. Godon

    Office National d'Études et de Recherches Aérospatiales, France

    4 publications · 87 citations

    4

    h-index

  5. JD
    J. Duterque

    Office National d'Études et de Recherches Aérospatiales, France

    3 publications · 77 citations

    3

    h-index

1–5 of 117

Venues

  1. Journal of Propulsion and Power

    17 publications · 437 citations

    12

    h-index

  2. AIAA Journal

    10 publications · 427 citations

    10

    h-index

  3. Combustion and Flame

    6 publications · 129 citations

    6

    h-index

  4. Symposium (International) on Combustion

    3 publications · 120 citations

    3

    h-index

  5. Journal of Spacecraft and Rockets

    3 publications · 71 citations

    3

    h-index

1–5