Numerical study on joined : wing aircraft

A joined wing aircraft model B150 and conventional aircraft model D150 was selected to be examined. Fluent was used to conduct Reynolds-Averaged Naiver-Stokes simulation on the aerodynamic characteristics, such as lift and drag under varied angle of attack, under transonic speed. The lift and drag c...

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Main Author:	Singaravelan
Other Authors:	New Tze How, Daniel
Format:	Final Year Project
Language:	English
Published:	Nanyang Technological University 2020
Subjects:	Engineering::Mechanical engineering
Online Access:	https://hdl.handle.net/10356/145590
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Institution:	Nanyang Technological University
Language:	English

id	sg-ntu-dr.10356-145590
record_format	dspace
spelling	sg-ntu-dr.10356-1455902023-03-04T19:47:25Z Numerical study on joined : wing aircraft Singaravelan New Tze How, Daniel School of Mechanical and Aerospace Engineering DTHNEW@ntu.edu.sg Engineering::Mechanical engineering A joined wing aircraft model B150 and conventional aircraft model D150 was selected to be examined. Fluent was used to conduct Reynolds-Averaged Naiver-Stokes simulation on the aerodynamic characteristics, such as lift and drag under varied angle of attack, under transonic speed. The lift and drag coefficient were compared against different angle of attack ranging from 0°–20° degrees.The B150 model have many advantages over conventionalD150 model, discussion was done on those advantages and a study of numerical analysis on its aerodynamics was done.The comparison made between model B150 joined wing aircraft and D150 conventional aircraft indicates that a joined wing configuration is an alternative from the D150conventional aircraft. Bachelor of Engineering (Mechanical Engineering) 2020-12-30T01:24:10Z 2020-12-30T01:24:10Z 2020 Final Year Project (FYP) https://hdl.handle.net/10356/145590 en application/pdf Nanyang Technological University
institution	Nanyang Technological University
building	NTU Library
continent	Asia
country	Singapore Singapore
content_provider	NTU Library
collection	DR-NTU
language	English
topic	Engineering::Mechanical engineering
spellingShingle	Engineering::Mechanical engineering Singaravelan Numerical study on joined : wing aircraft
description	A joined wing aircraft model B150 and conventional aircraft model D150 was selected to be examined. Fluent was used to conduct Reynolds-Averaged Naiver-Stokes simulation on the aerodynamic characteristics, such as lift and drag under varied angle of attack, under transonic speed. The lift and drag coefficient were compared against different angle of attack ranging from 0°–20° degrees.The B150 model have many advantages over conventionalD150 model, discussion was done on those advantages and a study of numerical analysis on its aerodynamics was done.The comparison made between model B150 joined wing aircraft and D150 conventional aircraft indicates that a joined wing configuration is an alternative from the D150conventional aircraft.
author2	New Tze How, Daniel
author_facet	New Tze How, Daniel Singaravelan
format	Final Year Project
author	Singaravelan
author_sort	Singaravelan
title	Numerical study on joined : wing aircraft
title_short	Numerical study on joined : wing aircraft
title_full	Numerical study on joined : wing aircraft
title_fullStr	Numerical study on joined : wing aircraft
title_full_unstemmed	Numerical study on joined : wing aircraft
title_sort	numerical study on joined : wing aircraft
publisher	Nanyang Technological University
publishDate	2020
url	https://hdl.handle.net/10356/145590
_version_	1759855625872867328

Numerical study on joined : wing aircraft

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