Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail

Performing the biomimetic morphing method on a Micro Air Vehicle (MAV) wing is very challenging tasks due to the MAV wing size limitation, limited energy budgets, complicated morphing mechanism and complex aeroelastic interactions. These issues had restricted the application of morphing wing on MAV...

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Bibliographic Details
Main Author:	Ismail, Noor Iswadi
Format:	Book Section
Language:	English
Published:	Institute of Graduate Studies, UiTM 2015
Subjects:	Malaysia
Online Access:	http://ir.uitm.edu.my/id/eprint/19558/ http://ir.uitm.edu.my/id/eprint/19558/1/ABS_NOOR%20ISWADI%20ISMAIL%20TDRA%20VOL%208%20IGS%2015.pdf

id	uitm-19558
recordtype	eprints
spelling	uitm-195582018-06-12T02:27:56Z http://ir.uitm.edu.my/id/eprint/19558/ Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail Ismail, Noor Iswadi Malaysia Performing the biomimetic morphing method on a Micro Air Vehicle (MAV) wing is very challenging tasks due to the MAV wing size limitation, limited energy budgets, complicated morphing mechanism and complex aeroelastic interactions. These issues had restricted the application of morphing wing on MAV wing platform. As a result, the impact of twist morphing on MAV wing aerodynamics and structural performances was not fully understood. Thus, this thesis presents the investigation of wing structural, aerodynamics performance and flow structure formations on a basic twist morphing MAV wing named as Twist Morphing wing. A series of morphing force intensity was imposed on Twist Morphing wing design to elucidate the impact of twist morphing mobility. Fully coupled Fluid-Structure Interaction (FSI) simulation is the main methodology used in this works. The wing structural and airflow field problems over Twist Morphing wing were solved based on a three-dimensional (3D) linear quasi- static structural coupled with steady state, incompressible Reynolds Averaged Navier Stokes - Shear Stress Turbulence (RANS–SST) flow… Institute of Graduate Studies, UiTM 2015 Book Section PeerReviewed text en http://ir.uitm.edu.my/id/eprint/19558/1/ABS_NOOR%20ISWADI%20ISMAIL%20TDRA%20VOL%208%20IGS%2015.pdf Ismail, Noor Iswadi (2015) Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail. In: The Doctoral Research Abstracts. IGS Biannual Publication, 8 (8). Institute of Graduate Studies, UiTM, Shah Alam.
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Teknologi MARA
building	UiTM Institutional Repository
collection	Online Access
language	English
topic	Malaysia
spellingShingle	Malaysia Ismail, Noor Iswadi Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail
description	Performing the biomimetic morphing method on a Micro Air Vehicle (MAV) wing is very challenging tasks due to the MAV wing size limitation, limited energy budgets, complicated morphing mechanism and complex aeroelastic interactions. These issues had restricted the application of morphing wing on MAV wing platform. As a result, the impact of twist morphing on MAV wing aerodynamics and structural performances was not fully understood. Thus, this thesis presents the investigation of wing structural, aerodynamics performance and flow structure formations on a basic twist morphing MAV wing named as Twist Morphing wing. A series of morphing force intensity was imposed on Twist Morphing wing design to elucidate the impact of twist morphing mobility. Fully coupled Fluid-Structure Interaction (FSI) simulation is the main methodology used in this works. The wing structural and airflow field problems over Twist Morphing wing were solved based on a three-dimensional (3D) linear quasi- static structural coupled with steady state, incompressible Reynolds Averaged Navier Stokes - Shear Stress Turbulence (RANS–SST) flow…
format	Book Section
author	Ismail, Noor Iswadi
author_facet	Ismail, Noor Iswadi
author_sort	Ismail, Noor Iswadi
title	Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail
title_short	Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail
title_full	Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail
title_fullStr	Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail
title_full_unstemmed	Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail
title_sort	aerodynamic performances of twist morphing mav wing / noor iswadi ismail
publisher	Institute of Graduate Studies, UiTM
publishDate	2015
url	http://ir.uitm.edu.my/id/eprint/19558/ http://ir.uitm.edu.my/id/eprint/19558/1/ABS_NOOR%20ISWADI%20ISMAIL%20TDRA%20VOL%208%20IGS%2015.pdf
first_indexed	2023-09-18T23:02:49Z
last_indexed	2023-09-18T23:02:49Z
_version_	1777418287042265088

Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail

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