Influence of Mountiing on the Accuracy of Piezoelectric Pressure Measurements for Hypersonic Boundary Layer Transition
Author:
Affiliation:
1. PCB Piezotronics, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-2292
Reference13 articles.
1. Boundary-Layer Instability Measurements in a Mach-6 Quiet Tunnel
2. Fluctuating wall pressures measured beneath a supersonic turbulent boundary layer
3. Berridge, D. C. (2015). Generating low-pressure shock waves for calibrating high-frequency pressure sensors. Ph.D. Dissertation,Purdue University, West LafayetteIndiana.
4. Hypersonic Wind-Tunnel Measurements of Boundary-Layer Pressure Fluctuations
5. Surface-Pressure Measurements of Second-Mode Instability in Quiet Hypersonic Flow
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