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New computational methods for the prediction and analysis of helicopter noise
1996
Aeroacoustics Conference
unpublished
Preserved Fulltext
This paper describes several new methods to predict and analyze rotorcraft noise. These methods are: 1) a combined computational fluid dynamics and Kirch-
doi:10.2514/6.1996-1696
fatcat:dk5q4milv5gi5bsydqltctehpu