Unstart Phenomena

Unstart Phenomena is a transient aerodynamic instability in scramjet propulsion systems characterized by the sudden detachment and upstream propagation of a shock train caused by adverse pressure gradients, leading to the collapse of supersonic airflow within the combustor and a subsequent loss of thrust generation.

69

Publications

3.3K

Citations

173

Authors

54

Institutions

Publications per year

2017–2026

13

Variants

Inlet Unstart

Authors

173

  1. NT
    Noel T. Clemens

    The University of Texas at Austin, United States

    8 publications · 698 citations

    8

    h-index

  2. JL
    Justin L. Wagner

    Sandia National Laboratories, United States

    7 publications · 685 citations

    7

    h-index

  3. TM
    Tohru Mitani

    Tohoku University, Japan

    6 publications · 267 citations

    6

    h-index

  4. DB
    Damiano Baccarella

    University of Illinois Urbana-Champaign, United States

    5 publications · 231 citations

    5

    h-index

  5. AV
    Agustin Valdivia

    The University of Texas at Austin, United States

    5 publications · 508 citations

    5

    h-index

1–5 of 173

Venues

  1. Journal of Propulsion and Power

    12 publications · 559 citations

    11

    h-index

  2. AIAA Journal

    7 publications · 792 citations

    7

    h-index

  3. Aerospace Science and Technology

    AST · 5 publications · 176 citations

    5

    h-index

  4. Physics of Fluids

    3 publications · 120 citations

    3

    h-index

  5. Journal of Aircraft

    3 publications · 132 citations

    3

    h-index

1–5