BOUNDARY ELEMENT METHOD FOR SUBSONIC COMPRESSIBLE FLOW OVER A WING USING VORTEX PARTICLE WAKES

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Bibliographic Details
Main Author:	FADLIKA, RIDWAN
Format:	Final Project
Language:	Indonesia
Online Access:	https://digilib.itb.ac.id/gdl/view/52779
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Institution:	Institut Teknologi Bandung
Language:	Indonesia

id	id-itb.:52779
spelling	id-itb.:527792021-02-22T00:00:00ZBOUNDARY ELEMENT METHOD FOR SUBSONIC COMPRESSIBLE FLOW OVER A WING USING VORTEX PARTICLE WAKES FADLIKA, RIDWAN Indonesia Final Project INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/52779 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
format	Final Project
author	FADLIKA, RIDWAN
spellingShingle	FADLIKA, RIDWAN BOUNDARY ELEMENT METHOD FOR SUBSONIC COMPRESSIBLE FLOW OVER A WING USING VORTEX PARTICLE WAKES
author_facet	FADLIKA, RIDWAN
author_sort	FADLIKA, RIDWAN
title	BOUNDARY ELEMENT METHOD FOR SUBSONIC COMPRESSIBLE FLOW OVER A WING USING VORTEX PARTICLE WAKES
title_short	BOUNDARY ELEMENT METHOD FOR SUBSONIC COMPRESSIBLE FLOW OVER A WING USING VORTEX PARTICLE WAKES
title_full	BOUNDARY ELEMENT METHOD FOR SUBSONIC COMPRESSIBLE FLOW OVER A WING USING VORTEX PARTICLE WAKES
title_fullStr	BOUNDARY ELEMENT METHOD FOR SUBSONIC COMPRESSIBLE FLOW OVER A WING USING VORTEX PARTICLE WAKES
title_full_unstemmed	BOUNDARY ELEMENT METHOD FOR SUBSONIC COMPRESSIBLE FLOW OVER A WING USING VORTEX PARTICLE WAKES
title_sort	boundary element method for subsonic compressible flow over a wing using vortex particle wakes
url	https://digilib.itb.ac.id/gdl/view/52779
_version_	1822929129820913664

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