Publication:
Experimental study of UAV propeller Thrust generation for various Propeller Blade-Span and the relation with mouth-ring

cris.author.scopus-author-id 57211608134
cris.author.scopus-author-id 55178487200
cris.author.scopus-author-id 57210118886
cris.author.scopus-author-id 57196198202
cris.author.scopus-author-id 57217631746
cris.author.scopus-author-id 57200576499
cris.author.scopus-author-id 55898485400
dc.contributor.author Othman M.N.K.
dc.contributor.author Razlan Z.M.
dc.contributor.author Wahid Z.A.
dc.contributor.author Shahriman A.B.
dc.contributor.author Zunaidi I.
dc.contributor.author Khairunizam W.
dc.contributor.author Noriman N.Z.
dc.date.accessioned 2024-12-14T01:29:35Z
dc.date.available 2024-12-14T01:29:35Z
dc.date.issued 2019-06-28
dc.description.abstract In this study, the main focus is to investigate the thrust generation of various propeller blade width-spans with the relation of mouth-ring application. By using the parameter, the thrust was calculated based on the value of velocity, voltage and rpm. The testing was performed in two condition that is with mouth-ring and without mouth-ring and 2 size of propeller been tested in this experiment. The application of mouth-ring is based on the gap between the wall of mouth-ring and the blade tip. There are 3 size of gap; 10mm, 8mm and 5mm. The result shows that 10mm mouth-ring have better thrust generation other than two gap. In addition, if compare to with and without mouth-ring, the application of mouth-ring also has proved it has a better thrust. Furthermore, the application of mouth-ring is evaluating to be good base on this study.
dc.identifier.doi 10.1088/1757-899X/557/1/012052
dc.identifier.scopus 2-s2.0-85069521395
dc.identifier.uri https://hdl.handle.net/20.500.14170/10383
dc.relation.grantno undefined
dc.relation.ispartof IOP Conference Series: Materials Science and Engineering
dc.relation.ispartofseries IOP Conference Series: Materials Science and Engineering
dc.relation.issn 17578981
dc.rights open access
dc.title Experimental study of UAV propeller Thrust generation for various Propeller Blade-Span and the relation with mouth-ring
dc.type Conference Proceeding
dspace.entity.type Publication
oaire.citation.issue 1
oaire.citation.volume 557
oairecerif.affiliation.orgunit Universiti Malaysia Perlis
oairecerif.affiliation.orgunit Universiti Malaysia Perlis
oairecerif.affiliation.orgunit Universiti Malaysia Perlis
oairecerif.affiliation.orgunit Universiti Malaysia Perlis
oairecerif.affiliation.orgunit University of Sunderland
oairecerif.affiliation.orgunit Universiti Malaysia Perlis
oairecerif.affiliation.orgunit Universiti Malaysia Perlis
oairecerif.citation.number 012052
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person.identifier.scopus-author-id 57211608134
person.identifier.scopus-author-id 55178487200
person.identifier.scopus-author-id 57210118886
person.identifier.scopus-author-id 57196198202
person.identifier.scopus-author-id 57217631746
person.identifier.scopus-author-id 57200576499
person.identifier.scopus-author-id 55898485400
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