Construct · 1 fields · 1 citations

Mack second mode: a standalone construct

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Aerodynamics

an acoustic-type instability of hypersonic boundary layers, trapped between the wall and the relative sonic line, that dominates transition at high Mach number.

In aerodynamics, Mack second mode refers to an acoustic-type instability of hypersonic boundary layers, trapped between the wall and the relative sonic line, that dominates transition at high Mach number. This meaning comes from Fedorov (2011) in Annual Review of Fluid Mechanics.[1]

Unit
Recovery means
Measured by

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Nearby constructs

boundary4 fields · 4 citationsjingle · one word, four constructs instability3 fields · 3 citationsjingle · one word, three constructs line4 fields · 7 citationsjingle · one word, four constructs

References

Fedorov, A. (2011). Transition and Stability of High-Speed Boundary Layers. Annual Review of Fluid Mechanics, 43(1), 79-95. https://doi.org/10.1146/annurev-fluid-122109-160750

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