Abstract
A data-driven model containing a symmetrical deep neural network is proposed to reconstruct the flow field structure in a cascade channel by measuring discrete pressure values on the wall of the supersonic cascade channel. The model designed is to demonstrate that the deep neural network can realize the reconstruction and prediction of the flow field structure in the supersonic cascade channel under complicated and changing working conditions. The dataset used for model training is derived from numerical simulation of the supersonic cascade channel. The symmetrical model includes a transposed convolution part and a conventional convolution part, which, respectively, implement up-sampling of the pressure data and further extraction of features. The generalization ability and scalability of the model are analyzed from the contour plots of the pressure and density gradient. In order to verify the ability of the model to reconstruct unknown operating conditions, the organizational form of the training set and testing set has been specially designed to achieve the ability of interpolating outwards. In the testing set, the symmetrical model has a certain ability to realize extrapolation and prediction, and the flow field structure can be accurately reconstructed by using the discrete pressure values on the wall surface of the cascade channel. Moreover, to accurately evaluate the regression model proposed by this study, the correlation analysis was also applied in this study. The results show that the worst linear correlation coefficient is 0.9848 in the testing set, indicating that the model has satisfactory ability to reconstruct and predict the flow field.
Highlights
The flow field structure and flow state in the cascade are critical to the proper operation of the compressor
The discrete pressure data of the inner wall surface obtained by steady numerical simulation were preprocessed as the input of the model, and the reconstructed flow field in the form of the pressure field or density gradient field were considered as the output of the model, to reconstruct the flow field using the discrete pressure value and obtain the macroscopic information of the entire flow field
The supersonic cascade used to obtain steady numerical simulation data was SAV21, which is a stator blade compressor designed by the German Aerospace Center for studying supersonic compressors
Summary
The flow field structure and flow state in the cascade are critical to the proper operation of the compressor. This paper will demonstrate from the perspective of numerical simulation that deep learning can realize the reconstruction and inversion of the flow field structure in the supersonic cascade channel under complex and variable working conditions. The input data of the symmetry model is the discrete wall pressure value of the supersonic cascade channel under complex and variable conditions. The results of the model training show that the symmetrical model can accurately reconstruct the flow field structure in the supersonic cascade channel under complex and variable conditions (different incoming Mach numbers and back pressures), both in terms of pressure field and density gradient field. SYMMETRICAL CNN-BASED PRESSURE-SHOCK WAVE SYSTEM STRUCTURE NETWORK INSIDE A SUPERSONIC CASCADE CHANNEL
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