Rocket Combustion Instability

Rocket Combustion Instability is a combustion instability phenomenon characterized by self-sustained, large-amplitude pressure oscillations occurring within the combustion chamber of a rocket engine, arising from detrimental coupling between unsteady heat release and acoustic modes of the system.

250

Publications

9.8K

Citations

444

Authors

139

Institutions

Publications per year

2017–2026

46

Variants

Combustion Instability In Rocket Engines

Authors

444

  1. JH
    Justin Hardi

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    13 publications · 425 citations

    13

    h-index

  2. GF
    Gary Flandro

    University of Tennessee at Knoxville, United States

    16 publications · 746 citations

    13

    h-index

  3. WA
    William Anderson

    Purdue University West Lafayette, United States

    15 publications · 720 citations

    13

    h-index

  4. MO
    Michael Oschwald

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    12 publications · 378 citations

    12

    h-index

  5. FE
    F. E. C. Culick

    California Institute of Technology, United States

    10 publications · 853 citations

    10

    h-index

1–5 of 444

Venues

  1. Journal of Propulsion and Power

    54 publications · 2.5K citations

    28

    h-index

  2. AIAA Journal

    36 publications · 1.4K citations

    21

    h-index

  3. Symposium (International) on Combustion

    10 publications · 507 citations

    10

    h-index

  4. Acta Astronautica

    9 publications · 286 citations

    9

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 7 publications · 657 citations

    7

    h-index

1–5