MODEL TRANSMISI KEBISINGAN DARI PROPELLER KE KABIN PESAWAT
In this thesis, a model of noise transmission from propeller into the aircraft cabin is constructed. Noise transmission phenomenon is then considered as an acoustic wave problem. The model is intended to describe the suppress of noise due to the aircraft wall. Simulations show how acoustic wave p...
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id-itb.:339312019-01-31T10:23:12ZMODEL TRANSMISI KEBISINGAN DARI PROPELLER KE KABIN PESAWAT Turnip, Peri Matematika Indonesia Theses Noise, GA, Absorption, Passive Noise control, Waves, Mathematical models. INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/33931 In this thesis, a model of noise transmission from propeller into the aircraft cabin is constructed. Noise transmission phenomenon is then considered as an acoustic wave problem. The model is intended to describe the suppress of noise due to the aircraft wall. Simulations show how acoustic wave propagates from propeller toward the cabin. The noise which transmit into the cabin will be damped by aircraft wall. The maximum amplitude of acoustic wave propagates in the cabin is very important indicator of the aircraft wall quality. Genetic algorithm(GA) optimization method is used to nd optimum value of absorption coecient of aircraft wall to produce amplitude very close to the maximum expected amplitude in cabin. . text |
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Matematika Turnip, Peri MODEL TRANSMISI KEBISINGAN DARI PROPELLER KE KABIN PESAWAT |
description |
In this thesis, a model of noise transmission from propeller into the aircraft cabin
is constructed. Noise transmission phenomenon is then considered as an acoustic
wave problem. The model is intended to describe the suppress of noise due to the
aircraft wall. Simulations show how acoustic wave propagates from propeller toward
the cabin. The noise which transmit into the cabin will be damped by aircraft wall.
The maximum amplitude of acoustic wave propagates in the cabin is very important
indicator of the aircraft wall quality. Genetic algorithm(GA) optimization method
is used to nd optimum value of absorption coecient of aircraft wall to produce
amplitude very close to the maximum expected amplitude in cabin. . |
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Theses |
author |
Turnip, Peri |
author_facet |
Turnip, Peri |
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Turnip, Peri |
title |
MODEL TRANSMISI KEBISINGAN DARI PROPELLER KE KABIN PESAWAT |
title_short |
MODEL TRANSMISI KEBISINGAN DARI PROPELLER KE KABIN PESAWAT |
title_full |
MODEL TRANSMISI KEBISINGAN DARI PROPELLER KE KABIN PESAWAT |
title_fullStr |
MODEL TRANSMISI KEBISINGAN DARI PROPELLER KE KABIN PESAWAT |
title_full_unstemmed |
MODEL TRANSMISI KEBISINGAN DARI PROPELLER KE KABIN PESAWAT |
title_sort |
model transmisi kebisingan dari propeller ke kabin pesawat |
url |
https://digilib.itb.ac.id/gdl/view/33931 |
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