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March 3, 2026Aerospace Science and Technology2 citations

Effects of boundary layer transition on the unsteady SWBLI past the forebody and intake at hypersonic speed

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YYYijiang YangZXZhixiang Xiao

Key Points

  • SWBLI is significantly affected by boundary layer transition, impacting its stability.
  • The transition influences the flow dynamics around the forebody and intake at hypersonic speeds.
  • Observational analysis focused on hypersonic conditions to study boundary layer effects.
  • Results highlight the importance of understanding boundary layer transitions for hypersonic vehicle design.
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Cite This Study

Yang et al. (2026) studied this question.

synapsesocial.com/papers/69a76184c6e9836116a2f87dhttps://doi.org/10.1016/j.ast.2026.111922
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