NASA NTRS · 19820050734
Turbulence amplification in shock-wave boundary-layer interaction
Abstract
Attention is directed to the acoustics research of the 1950s and 1960s for guidance in understanding and quantizing the turbulence amplification that can occur in regions of shock-wave boundary-layer interaction. Three primary turbulence amplifier-generator mechanisms are identified and shown, by linear analysis, to be responsible for turbulence amplification across a shock wave in excess of 100% of the incident turbulence intensity.
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Anyiwo, J. C., Bushnell, D. M.. 1982-07-01. Turbulence amplification in shock-wave boundary-layer interaction. https://ntrs.nasa.gov/citations/19820050734
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