Zhang, Y., Wang, F. Y., & Hardin, J. C. (2003). Spectral characteristics of wake vortex sound during roll-up (Report No. NASA/CR-2003-212673). United States. National Aeronautics and Space Administration. https://rosap.ntl.bts.gov/view/dot/9667
Zhang, Yan, Frank Y. Wang, and J. C. Hardin. Spectral characteristics of wake vortex sound during roll-up. Report no. NASA/CR-2003-212673. United States. National Aeronautics and Space Administration, 2003. https://rosap.ntl.bts.gov/view/dot/9667.
Zhang, Yan, et al. Spectral characteristics of wake vortex sound during roll-up. United States. National Aeronautics and Space Administration, 2003, Report no. NASA/CR-2003-212673, ROSA P. https://rosap.ntl.bts.gov/view/dot/9667.
This report presents an analysis of the sound spectra generated by a trailing aircraft vortex during its rolling-up process. The
;
study demonstrates that a rolling-up vortex could produce low frequency (less than 100 Hz) sound with very high intensity (60
;
dB above threshold of human hearing) at a distance of 200 feet from the vortex core. The spectrum then drops off rapidly
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thereafter. The study suggests that acoustic sensors operating at low frequency band could be profitably deployed for detecting
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the vortex sound during the rolling-up process.
Zhang, Y., Wang, F. Y., & Hardin, J. C. (2003). Spectral characteristics of wake vortex sound during roll-up (Report No. NASA/CR-2003-212673). United States. National Aeronautics and Space Administration. https://rosap.ntl.bts.gov/view/dot/9667
Zhang, Yan, Frank Y. Wang, and J. C. Hardin. Spectral characteristics of wake vortex sound during roll-up. Report no. NASA/CR-2003-212673. United States. National Aeronautics and Space Administration, 2003. https://rosap.ntl.bts.gov/view/dot/9667.
Zhang, Yan, et al. Spectral characteristics of wake vortex sound during roll-up. United States. National Aeronautics and Space Administration, 2003, Report no. NASA/CR-2003-212673, ROSA P. https://rosap.ntl.bts.gov/view/dot/9667.
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