Correlation measurement of supersonic flow pulsations and boundary layer disturbances in wind tunnel at Mach 2
Author:
Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0028401
Reference12 articles.
1. Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition
2. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition
3. G. S. Jones, P. C. Stainback, C. D. Harris, C. W. Brooks, and S. J. Clukey, AIAA-89-0150 (1989).
4. Correlation Measurement in a Turbulent Flow using High-Speed Computing Methods
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1. On the Methodology for Estimating the Relationship of Disturbances Using Digital Signal Processing in Relation to Measurements in Supersonic Flows;SIBERIAN JOURNAL OF PHYSICS;2023-05-10
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