Supersonic Inlets

Supersonic Inlets is a type of aerodynamic inlet designed to efficiently decelerate and compress supersonic airflow to subsonic speeds for entry into aircraft engines, distinguished by its capability to manage shock waves and maintain stable flow under supersonic flight conditions.

279

Publications

8.8K

Citations

588

Authors

182

Institutions

Publications per year

2017–2026

43

Variants

Supersonic Air Intakes

Authors

588

  1. JW
    John W. Slater

    Glenn Research Center, United States

    14 publications · 381 citations

    14

    h-index

  2. SH
    Stefanie Hirt

    Glenn Research Center, United States

    9 publications · 180 citations

    9

    h-index

  3. MR
    M. R. Soltani

    Sharif University of Technology, Iran

    8 publications · 162 citations

    8

    h-index

  4. MF
    Mohammad Farahani

    Sharif University of Technology, Iran

    8 publications · 191 citations

    8

    h-index

  5. TC
    Timothy Conners

    Glenn Research Center, United States

    7 publications · 181 citations

    7

    h-index

1–5 of 588

Venues

  1. Journal of Propulsion and Power

    30 publications · 1K citations

    21

    h-index

  2. AIAA Journal

    24 publications · 1.2K citations

    18

    h-index

  3. Aerospace Science and Technology

    AST · 17 publications · 443 citations

    15

    h-index

  4. Journal of Aircraft

    18 publications · 584 citations

    14

    h-index

  5. 7

    h-index

1–5