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IMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLES

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dc.contributor.authorRazak N.A.en_US
dc.contributor.authorAbas A.en_US
dc.contributor.authorItam Z.en_US
dc.contributor.authorid52364538900en_US
dc.contributor.authorid56893346700en_US
dc.contributor.authorid55102723400en_US
dc.date.accessioned2023-05-29T07:27:37Z
dc.date.available2023-05-29T07:27:37Z
dc.date.issued2019
dc.description.abstractUnmanned 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.en_US
dc.description.natureFinalen_US
dc.identifier.epage166
dc.identifier.scopus2-s2.0-85144980697
dc.identifier.spage149
dc.identifier.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-85144980697&partnerID=40&md5=479fd91d8b95f99e0157a42105506add
dc.identifier.urihttps://irepository.uniten.edu.my/handle/123456789/24828
dc.publisherNova Science Publishers, Inc.en_US
dc.sourceScopus
dc.sourcetitleAdvances in Aerospace Science and Technology: Part II
dc.titleIMPORTANT AERODYNAMIC PARAMETERS OF FLAPPING-WING UNMANNED AERIAL VEHICLESen_US
dc.typeBook Chapteren_US
dspace.entity.typePublication
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