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

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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Bibliographic Details
Main Author: Ahmad, Muhammad Aiman
Format: Thesis
Language:English
Published: 2019
Online Access:https://ir.uitm.edu.my/id/eprint/87856/1/87856.pdf
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spelling my-uitm-ir.878562024-04-11T23:39:16Z The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad 2019 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 https://ir.uitm.edu.my/id/eprint/87856/ https://ir.uitm.edu.my/id/eprint/87856/1/87856.pdf text en public masters Universiti Teknologi MARA (UiTM) Faculty of Mechanical Engineering Mohd Nasir, Rizal Effendy
institution Universiti Teknologi MARA
collection UiTM Institutional Repository
language English
advisor Mohd Nasir, Rizal Effendy
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
qualification_level Master's degree
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
granting_institution Universiti Teknologi MARA (UiTM)
granting_department Faculty of Mechanical Engineering
publishDate 2019
url https://ir.uitm.edu.my/id/eprint/87856/1/87856.pdf
_version_ 1804889792800882688

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