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Obtaining phase velocity of turbulent boundary layer pressure fluctuations at high subsonic Mach number from wind tunnel data affected by strong background noise
Research article (Journal of Sound and Vibration, 2017) · cited 18× · AI/ML
Obtaining phase velocity of turbulent boundary layer pressure fluctuations at high subsonic Mach number from wind tunnel data affected by strong background noise
Summary
Obtaining phase velocity of turbulent boundary layer pressure fluctuations at high subsonic Mach number from wind tunnel data affected by strong background noise is a scholarly article[1].
Key Facts
Obtaining phase velocity of turbulent boundary layer pressure fluctuations at high subsonic Mach number from wind tunnel data affected by strong background noise's instance of is recorded as scholarly article[2].
References
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APA4ort.xyz Knowledge Graph. (2026). Obtaining phase velocity of turbulent boundary layer pressure fluctuations at high subsonic Mach number from wind tunnel data affected by strong background noise. Retrieved May 24, 2026, from https://4ort.xyz/entity/obtaining-phase-velocity-of-turbulent-boundary-layer-pressure-fluctuations-at-high-subsonic-mach-number-from-wind-tunnel
MLA“Obtaining phase velocity of turbulent boundary layer pressure fluctuations at high subsonic Mach number from wind tunnel data affected by strong background noise.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/obtaining-phase-velocity-of-turbulent-boundary-layer-pressure-fluctuations-at-high-subsonic-mach-number-from-wind-tunnel.
BibTeX@misc{4ortxyz_obtaining-phase-velocity-of-turbulent-boundary-layer-pressure-fluctuations-at-high-subsonic-mach-number-from-wind-tunnel_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Obtaining phase velocity of turbulent boundary layer pressure fluctuations at high subsonic Mach number from wind tunnel data affected by strong background noise}}, year = {2026}, url = {https://4ort.xyz/entity/obtaining-phase-velocity-of-turbulent-boundary-layer-pressure-fluctuations-at-high-subsonic-mach-number-from-wind-tunnel}, note = {Accessed: 2026-05-24}}
LLM promptAccording to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): Obtaining phase velocity of turbulent boundary layer pressure fluctuations at high subsonic Mach number from wind tunnel data affected by strong background noise — https://4ort.xyz/entity/obtaining-phase-velocity-of-turbulent-boundary-layer-pressure-fluctuations-at-high-subsonic-mach-number-from-wind-tunnel (retrieved 2026-05-24)
