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The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad

The study on BWB UAV begins in UiTM in 2005, focused on the design and fundamental aerodynamics and flight dynamics of small Blended Wing-Body (BWB). The objective of this research was to measure the aerodynamic characteristics on BWB Baseline 7 aircraft. It also to analyse pitching, rolling, and ya...

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Main Author: Ahmad, Muhammad Aiman
Format: Thesis
Language:English
Published: 2019
Online Access:https://ir.uitm.edu.my/id/eprint/87856/1/87856.pdf
https://ir.uitm.edu.my/id/eprint/87856/
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id my.uitm.ir.87856
record_format eprints
spelling my.uitm.ir.878562024-08-13T08:55:39Z https://ir.uitm.edu.my/id/eprint/87856/ The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad Ahmad, Muhammad Aiman The study on BWB UAV begins in UiTM in 2005, focused on the design and fundamental aerodynamics and flight dynamics of small Blended Wing-Body (BWB). The objective of this research was to measure the aerodynamic characteristics on BWB Baseline 7 aircraft. It also to analyse pitching, rolling, and yawing moment, on the BWB Baseline 7 due to four elevon configuration. The objective was also to determine the control surface configuration for -30, 0, and +30 deflection angle of control surface. 2019 Thesis NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/87856/1/87856.pdf The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad. (2019) Masters thesis, thesis, Universiti Teknologi MARA (UiTM). <http://terminalib.uitm.edu.my/87856.pdf>
institution Universiti Teknologi Mara
building Tun Abdul Razak Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Mara
content_source UiTM Institutional Repository
url_provider http://ir.uitm.edu.my/
language English
description The study on BWB UAV begins in UiTM in 2005, focused on the design and fundamental aerodynamics and flight dynamics of small Blended Wing-Body (BWB). The objective of this research was to measure the aerodynamic characteristics on BWB Baseline 7 aircraft. It also to analyse pitching, rolling, and yawing moment, on the BWB Baseline 7 due to four elevon configuration. The objective was also to determine the control surface configuration for -30, 0, and +30 deflection angle of control surface.
format Thesis
author Ahmad, Muhammad Aiman
spellingShingle Ahmad, Muhammad Aiman
The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad
author_facet Ahmad, Muhammad Aiman
author_sort Ahmad, Muhammad Aiman
title The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad
title_short The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad
title_full The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad
title_fullStr The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad
title_full_unstemmed The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad
title_sort effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less bwb / muhammad aiman ahmad
publishDate 2019
url https://ir.uitm.edu.my/id/eprint/87856/1/87856.pdf
https://ir.uitm.edu.my/id/eprint/87856/
_version_ 1808975929603522560
score 13.211869

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