Inlet Compression

Inlet Compression is a supersonic airflow deceleration process in which the incoming air is compressed through shock waves and boundary layer interactions within the engine inlet, enabling efficient pressure rise ahead of the combustor in scramjet engines.

146

Publications

5K

Citations

348

Authors

131

Institutions

Publications per year

2017–2026

26

Authors

348

  1. AG
    Ali Gülhan

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

    10 publications · 327 citations

    10

    h-index

  2. ML
    Mark Lewis

    University of Maryland, College Park, United States

    4 publications · 86 citations

    4

    h-index

  3. OH
    Oliver Hohn

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

    4 publications · 82 citations

    4

    h-index

  4. II
    I. I. Mazhul

    Institute of Theoretical and Applied Mechanics, Russia

    3 publications · 54 citations

    3

    h-index

  5. RW
    R. W. Cubbison

    Glenn Research Center, United States

    3 publications · 67 citations

    3

    h-index

1–5 of 348

Venues

  1. Journal of Propulsion and Power

    18 publications · 765 citations

    15

    h-index

  2. AIAA Journal

    14 publications · 775 citations

    13

    h-index

  3. NASA Technical Reports Server (NASA)

    Repository · 6 publications · 103 citations

    6

    h-index

  4. Acta Astronautica

    5 publications · 118 citations

    5

    h-index

  5. Aerospace Science and Technology

    AST · 4 publications · 90 citations

    4

    h-index

1–5