Hypersonic Testing

Hypersonic Testing is a type of aerodynamic testing that involves the experimental evaluation of flow characteristics and vehicle performance at speeds exceeding Mach 5, where high-temperature effects, real gas dynamics, and shock wave interactions dominate the flow regime.

1K

Publications

33K

Citations

2.1K

Authors

409

Institutions

Publications per year

2017–2026

165

Authors

2.1K

  1. RL
    Roger L. Kimmel

    United States Air Force Research Laboratory, United States

    32 publications · 1.3K citations

    23

    h-index

  2. SP
    Steven P. Schneider

    Purdue University West Lafayette, United States

    27 publications · 1.5K citations

    20

    h-index

  3. TH
    Thomas Horvath

    Langley Research Center, United States

    18 publications · 647 citations

    14

    h-index

  4. TJ
    Thomas J. Juliano

    University of Notre Dame, United States

    17 publications · 584 citations

    14

    h-index

  5. MH
    Michael Holden

    Calspan-University of Buffalo Research Center, United States

    19 publications · 612 citations

    14

    h-index

1–5 of 2.1K

Venues

  1. Journal of Spacecraft and Rockets

    80 publications · 3.1K citations

    33

    h-index

  2. AIAA Journal

    93 publications · 3.1K citations

    32

    h-index

  3. Acta Astronautica

    27 publications · 1.2K citations

    19

    h-index

  4. Journal of Propulsion and Power

    20 publications · 980 citations

    18

    h-index

  5. Aerospace Science and Technology

    AST · 21 publications · 812 citations

    17

    h-index

1–5