A CONCEPTUAL DESIGN OF A 20-SEATER WING IN SURFACE EFFECT CRAFT “WISE-20”

Wing in Surface Effect (WiSE) or Wing in Ground Effect (WiG) craft is an air vehicle flying nearby surface to obtain higher aerodynamic performance, such as lift to drag ratio. The effect exists in between the altitude of less than one wing span from the surface. Based on Indonesia’s development in...

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Main Author: Indawan Utomo, Ridho
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/33629
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:33629
spelling id-itb.:336292019-01-28T09:40:19ZA CONCEPTUAL DESIGN OF A 20-SEATER WING IN SURFACE EFFECT CRAFT “WISE-20” Indawan Utomo, Ridho Indonesia Final Project wing in surface effect, ground effect, conceptual design, preliminary study, WiSE geometry, WiSE configuration, WiSE 3D model. INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/33629 Wing in Surface Effect (WiSE) or Wing in Ground Effect (WiG) craft is an air vehicle flying nearby surface to obtain higher aerodynamic performance, such as lift to drag ratio. The effect exists in between the altitude of less than one wing span from the surface. Based on Indonesia’s development in infrastructure and transportation capability, WiSE craft may become one of supporting vehicle to increase mobility in covering off grid and small islands in Indonesia. Previously, WiSE craft has been developed by the Agency for the Assessment and Application of Technology (BPPT) and Bandung Institute of Technology (ITB), building an eight-seater configuration (WiSE 8 Craft). Even though the project was discontinued, until now WiSE crafts are developed extensively by other countries. Hence, this thesis explores WiSE craft of a 20-seater configuration to become a future study of a bigger WiSE craft. This thesis covers the conceptual design phase that consists of determining the geometry, propulsion used, and components’ configuration. Each of the criteria has to be validated by available data and analysis, e.g. aerodynamic analysis. Furthermore, the comparable data will be generated from similar existing WiSE crafts in order to produce a feasible design. The design follows the guideline of aircraft design’s handbook with modified calculation for its hydrodynamic operation. The design is then expressed in 3D model with software CATIA V5R21. The design shows promising result even though its performance only reaches as high as 15 for its lift to drag ratio. The design fulfilled the DRO created based on similar WiSE crafts. However, structural aspect could not be modeled due to its limitation in conceptual design phase. To improve the design, each assumptions and judgements has to be verified with existing data and available analysis. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description Wing in Surface Effect (WiSE) or Wing in Ground Effect (WiG) craft is an air vehicle flying nearby surface to obtain higher aerodynamic performance, such as lift to drag ratio. The effect exists in between the altitude of less than one wing span from the surface. Based on Indonesia’s development in infrastructure and transportation capability, WiSE craft may become one of supporting vehicle to increase mobility in covering off grid and small islands in Indonesia. Previously, WiSE craft has been developed by the Agency for the Assessment and Application of Technology (BPPT) and Bandung Institute of Technology (ITB), building an eight-seater configuration (WiSE 8 Craft). Even though the project was discontinued, until now WiSE crafts are developed extensively by other countries. Hence, this thesis explores WiSE craft of a 20-seater configuration to become a future study of a bigger WiSE craft. This thesis covers the conceptual design phase that consists of determining the geometry, propulsion used, and components’ configuration. Each of the criteria has to be validated by available data and analysis, e.g. aerodynamic analysis. Furthermore, the comparable data will be generated from similar existing WiSE crafts in order to produce a feasible design. The design follows the guideline of aircraft design’s handbook with modified calculation for its hydrodynamic operation. The design is then expressed in 3D model with software CATIA V5R21. The design shows promising result even though its performance only reaches as high as 15 for its lift to drag ratio. The design fulfilled the DRO created based on similar WiSE crafts. However, structural aspect could not be modeled due to its limitation in conceptual design phase. To improve the design, each assumptions and judgements has to be verified with existing data and available analysis.
format Final Project
author Indawan Utomo, Ridho
spellingShingle Indawan Utomo, Ridho
A CONCEPTUAL DESIGN OF A 20-SEATER WING IN SURFACE EFFECT CRAFT “WISE-20”
author_facet Indawan Utomo, Ridho
author_sort Indawan Utomo, Ridho
title A CONCEPTUAL DESIGN OF A 20-SEATER WING IN SURFACE EFFECT CRAFT “WISE-20”
title_short A CONCEPTUAL DESIGN OF A 20-SEATER WING IN SURFACE EFFECT CRAFT “WISE-20”
title_full A CONCEPTUAL DESIGN OF A 20-SEATER WING IN SURFACE EFFECT CRAFT “WISE-20”
title_fullStr A CONCEPTUAL DESIGN OF A 20-SEATER WING IN SURFACE EFFECT CRAFT “WISE-20”
title_full_unstemmed A CONCEPTUAL DESIGN OF A 20-SEATER WING IN SURFACE EFFECT CRAFT “WISE-20”
title_sort conceptual design of a 20-seater wing in surface effect craft “wise-20”
url https://digilib.itb.ac.id/gdl/view/33629
_version_ 1821996560792158208