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This paper presents an experimental study of laminar-to-turbulent boundary-layer transition in a circular duct at high supersonic Mach number. The experiments were conducted as an essential precurs... Click to show full abstract
This paper presents an experimental study of laminar-to-turbulent boundary-layer transition in a circular duct at high supersonic Mach number. The experiments were conducted as an essential precurs...
Keywords:
transition;
combustor transition;
transition lengths;
circular scramjet;
lengths mach;
scramjet combustor
Journal Title: AIAA Journal
Year Published: 2020
Link to full text (if available)
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Journal Title: AIAA Journal
Year Published: 2020
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!