DEVELOPMENT OF SURROGATE MODEL USING DEEP LEARNING AND PROPER ORTHOGONAL DECOMPOSITION METHOD ON AEROELASTIC DATA
Where non-linear aerodynamics sets a precedent in the governing flow, to which the transonic mach regime is concerned, producing aeroelastic models under these conditions is very expensive. This thesis investigates the utilization of Deep Learning to produce a surrogate model response surface bas...
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Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/70223 |
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Institution: | Institut Teknologi Bandung |
Language: | Indonesia |