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IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES

Unmanned aerial vehicles (UAVs) with flapping wings have been the focus of many recent studies due to their numerous applications. This chapter emphasises the essential parameters for the development and evaluation of flapping-wing UAVs. These parameters should be considered to successfully design f...

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Main Authors: Razak N.A., Abas A., Itam Z.
Other Authors: 52364538900
Format: Book Chapter
Published: Nova Science Publishers, Inc. 2023
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id my.uniten.dspace-24828
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spelling my.uniten.dspace-248282023-05-29T15:27:38Z IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES Razak N.A. Abas A. Itam Z. 52364538900 56893346700 55102723400 Unmanned aerial vehicles (UAVs) with flapping wings have been the focus of many recent studies due to their numerous applications. This chapter emphasises the essential parameters for the development and evaluation of flapping-wing UAVs. These parameters should be considered to successfully design flapping-wing UAVs. This chapter provides a short description of several topics related to flapping-wing flight and covers the basics of unsteady aerodynamic force generation.Subsequently, this chapter discusses important parameters of flappingwing aerial vehicles, such as Reynolds number, flow unsteadiness, wing geometry and flapping kinematics. This chapter also presents the modelling of flapping wing aerodynamics using quasi-steady approaches. � 2019 Nova Science Publishers, Inc. Final 2023-05-29T07:27:37Z 2023-05-29T07:27:37Z 2019 Book Chapter 2-s2.0-85144980697 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85144980697&partnerID=40&md5=479fd91d8b95f99e0157a42105506add https://irepository.uniten.edu.my/handle/123456789/24828 149 166 Nova Science Publishers, Inc. Scopus
institution Universiti Tenaga Nasional
building UNITEN Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tenaga Nasional
content_source UNITEN Institutional Repository
url_provider http://dspace.uniten.edu.my/
description Unmanned aerial vehicles (UAVs) with flapping wings have been the focus of many recent studies due to their numerous applications. This chapter emphasises the essential parameters for the development and evaluation of flapping-wing UAVs. These parameters should be considered to successfully design flapping-wing UAVs. This chapter provides a short description of several topics related to flapping-wing flight and covers the basics of unsteady aerodynamic force generation.Subsequently, this chapter discusses important parameters of flappingwing aerial vehicles, such as Reynolds number, flow unsteadiness, wing geometry and flapping kinematics. This chapter also presents the modelling of flapping wing aerodynamics using quasi-steady approaches. � 2019 Nova Science Publishers, Inc.
author2 52364538900
author_facet 52364538900
Razak N.A.
Abas A.
Itam Z.
format Book Chapter
author Razak N.A.
Abas A.
Itam Z.
spellingShingle Razak N.A.
Abas A.
Itam Z.
IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES
author_sort Razak N.A.
title IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES
title_short IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES
title_full IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES
title_fullStr IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES
title_full_unstemmed IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES
title_sort important aerodynamic parameters of flapping-wing unmanned aerial vehicles
publisher Nova Science Publishers, Inc.
publishDate 2023
_version_ 1806424275516653568
score 13.214268

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