Hypersonic Stability

Hypersonic Stability is a theoretical construct in aerodynamic stability analysis that specifically characterizes the tendency of a vehicle or flowfield to maintain or return to a desired trajectory or equilibrium state during atmospheric flight at Mach numbers typically exceeding five, distinguished from subsonic or supersonic stability by the dominant influence of high-temperature gas effects, viscous interactions, and shock wave nonlinearity.

382

Publications

16K

Citations

772

Authors

196

Institutions

Publications per year

2017–2026

115

Authors

772

  1. HL
    Helen L. Reed

    Texas A&M University, United States

    15 publications · 712 citations

    14

    h-index

  2. XZ
    Xiaolin Zhong

    University of California, Los Angeles, United States

    16 publications · 661 citations

    14

    h-index

  3. SP
    Steven P. Schneider

    Purdue University West Lafayette, United States

    16 publications · 1.1K citations

    14

    h-index

  4. RL
    Roger L. Kimmel

    United States Air Force Research Laboratory, United States

    12 publications · 872 citations

    11

    h-index

  5. AN
    A. N. Shiplyuk

    Institute of Theoretical and Applied Mechanics, Russia

    10 publications · 583 citations

    10

    h-index

1–5 of 772

Venues

  1. AIAA Journal

    31 publications · 1.6K citations

    23

    h-index

  2. Journal of Spacecraft and Rockets

    34 publications · 1.5K citations

    21

    h-index

  3. Aerospace Science and Technology

    AST · 20 publications · 797 citations

    17

    h-index

  4. Journal of Fluid Mechanics

    20 publications · 907 citations

    16

    h-index

  5. Physics of Fluids

    12 publications · 431 citations

    12

    h-index

1–5