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    In:  CASI
    Publication Date: 2006-04-17
    Description: Various parameters of helicopter rotor noise were considered. Impulsive noise, flow regions of a helicopter rotor, noise prediction, aspect ratio, blade tip shape and speed, and blade-vortex interaction noise were among the topics addressed. Recommendations were also given.
    Keywords: ACOUSTICS
    Type: NASA. Langley Research Center Rotorcraft Noise; p 203-218
    Format: text
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