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Estimating Helicopter Noise Abatement Information with Machine LearningMachine learning techniques are applied to the NASA Langley Research Center's expansive database of helicopter noise measurements containing over 1500 steady flight conditions for ten different helicopters. These techniques are then used to develop models capable of predicting the operating conditions under which significant Blade-Vortex Interaction noise will be generated for any conventional helicopter. A measure for quantifying the overall ground noise exposure of a particular helicopter operating condition is developed. This measure is then used to classify the measured flight conditions as noisy or not-noisy. These data are then parameterized on a nondimensional basis that defines the main rotor operating condition and are then scaled to remove bias. Several machine learning methods are then applied to these data. The developed models show good accuracy in identifying the noisy operating region for helicopters not included in the training data set. Noisy regions are accurately identified for a variety of different helicopters. One of these models is applied to estimate changes in the noisy operating region as vehicle drag and ambient atmospheric conditions are varied.
Document ID
20180006308
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Greenwood, Eric
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
October 16, 2018
Publication Date
May 14, 2018
Subject Category
Acoustics
Report/Patent Number
NF1676L-28372
Report Number: NF1676L-28372
Meeting Information
Meeting: American Helicopter Society (AHS) International Forum
Location: Phoenix, AZ
Country: United States
Start Date: May 14, 2018
End Date: May 17, 2018
Sponsors: Vertical Flight Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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