TY - GEN
T1 - A deep learning approach to jet noise prediction
AU - Tenney, Andrew S.
AU - Glauser, Mark N.
AU - Lewalle, Jacques
AU - Ruscher, Christopher J.
N1 - Publisher Copyright:
© 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2018
Y1 - 2018
N2 - This study is an exploration of a deep learning technique as it applies to jet noise prediction and modeling. A database was created describing the near-field and far-field conditions of a complex non-axisymmetric jet flow, with Mach numbers ranging from 1.0 to 1.6. The problem was posed as a form of multivariate nonlinear regression, and a Deep Neural Network (DNN) was used to create a model. Google’s TensorFlow was utilized in network construction and training, and a feature space consisting of plausible predictors of far-field directional SPL was defined, based on previous fundamental studies and jet noise scaling laws. The effects of feature space, learning rate, and network architecture modification were also studied and quantified. On average, the DNN was able to predict directional far-field SPL within ±0.75dB, surpassing our original goals. In addition, we suggest ways to extend this technique to encompass a greater range of nozzle geometries and flow conditions.
AB - This study is an exploration of a deep learning technique as it applies to jet noise prediction and modeling. A database was created describing the near-field and far-field conditions of a complex non-axisymmetric jet flow, with Mach numbers ranging from 1.0 to 1.6. The problem was posed as a form of multivariate nonlinear regression, and a Deep Neural Network (DNN) was used to create a model. Google’s TensorFlow was utilized in network construction and training, and a feature space consisting of plausible predictors of far-field directional SPL was defined, based on previous fundamental studies and jet noise scaling laws. The effects of feature space, learning rate, and network architecture modification were also studied and quantified. On average, the DNN was able to predict directional far-field SPL within ±0.75dB, surpassing our original goals. In addition, we suggest ways to extend this technique to encompass a greater range of nozzle geometries and flow conditions.
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U2 - 10.2514/6.2018-1736
DO - 10.2514/6.2018-1736
M3 - Conference contribution
AN - SCOPUS:85141597468
SN - 9781624105241
T3 - AIAA Aerospace Sciences Meeting, 2018
BT - AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aerospace Sciences Meeting, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -