Heat flux and skin friction on surface of a cone in supersonic flows

This report will look at analytical methods to calculate skin friction and heat flux on a cone. This will be done by assuming the flow to be either purely laminar and turbulent to provide information regarding these two basic cases. CFD will then be done in a similar fashion. This is toward the end...

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Bibliographic Details
Main Author:	T'ng, Alvin Weiheng
Other Authors:	School of Mechanical and Aerospace Engineering
Format:	Final Year Project
Language:	English
Published:	2012
Subjects:	DRNTU::Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Online Access:	http://hdl.handle.net/10356/50066
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Institution:	Nanyang Technological University
Language:	English

id	sg-ntu-dr.10356-50066
record_format	dspace
spelling	sg-ntu-dr.10356-500662023-03-04T19:26:03Z Heat flux and skin friction on surface of a cone in supersonic flows T'ng, Alvin Weiheng School of Mechanical and Aerospace Engineering Chue Shek Ming Randy DRNTU::Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics This report will look at analytical methods to calculate skin friction and heat flux on a cone. This will be done by assuming the flow to be either purely laminar and turbulent to provide information regarding these two basic cases. CFD will then be done in a similar fashion. This is toward the end of preparation for wind tunnel experiments. Bachelor of Engineering (Aerospace Engineering) 2012-05-29T06:57:07Z 2012-05-29T06:57:07Z 2012 2012 Final Year Project (FYP) http://hdl.handle.net/10356/50066 en Nanyang Technological University 137 p. application/pdf
institution	Nanyang Technological University
building	NTU Library
continent	Asia
country	Singapore Singapore
content_provider	NTU Library
collection	DR-NTU
language	English
topic	DRNTU::Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics
spellingShingle	DRNTU::Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics T'ng, Alvin Weiheng Heat flux and skin friction on surface of a cone in supersonic flows
description	This report will look at analytical methods to calculate skin friction and heat flux on a cone. This will be done by assuming the flow to be either purely laminar and turbulent to provide information regarding these two basic cases. CFD will then be done in a similar fashion. This is toward the end of preparation for wind tunnel experiments.
author2	School of Mechanical and Aerospace Engineering
author_facet	School of Mechanical and Aerospace Engineering T'ng, Alvin Weiheng
format	Final Year Project
author	T'ng, Alvin Weiheng
author_sort	T'ng, Alvin Weiheng
title	Heat flux and skin friction on surface of a cone in supersonic flows
title_short	Heat flux and skin friction on surface of a cone in supersonic flows
title_full	Heat flux and skin friction on surface of a cone in supersonic flows
title_fullStr	Heat flux and skin friction on surface of a cone in supersonic flows
title_full_unstemmed	Heat flux and skin friction on surface of a cone in supersonic flows
title_sort	heat flux and skin friction on surface of a cone in supersonic flows
publishDate	2012
url	http://hdl.handle.net/10356/50066
_version_	1759854945619673088

Heat flux and skin friction on surface of a cone in supersonic flows

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