Abstract
For experimental studies of transition from laminar to turbulent boundary layer flow it is important to know the ambient noise spectrum in the facility. In supersonic wind tunnels this is often assessed by measuring pitot pressure noise.
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References
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Hornung, H.G., Parziale, N.J. (2015). Spectral Characteristics of Pitot Noise. In: Bonazza, R., Ranjan, D. (eds) 29th International Symposium on Shock Waves 1. ISSW 2013. Springer, Cham. https://doi.org/10.1007/978-3-319-16835-7_64
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DOI: https://doi.org/10.1007/978-3-319-16835-7_64
Publisher Name: Springer, Cham
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