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Wavelet analysis of helicopter noise signal 被引量:1
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作者 ZHANG Qiang WANG Huaming HU Zhangwei (Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics Nanjing 210016) 《Chinese Journal of Acoustics》 2002年第1期23-29,共7页
Helicopter noise features under typical flight condition were investigated based on wavelet transform. The contribution of blade-vortex interaction (BVI) to helicopter noise and low frequency oscillations beat was sho... Helicopter noise features under typical flight condition were investigated based on wavelet transform. The contribution of blade-vortex interaction (BVI) to helicopter noise and low frequency oscillations beat was shown clearly from the detail of wavelet decomposition for helicopter noise signal. 展开更多
关键词 Wavelet analysis of helicopter noise signal
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