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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Bibliographic Details
Main Author: Iksan Musyahada, Kukuh
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