dc.contributor.authorIndra Gunawan
dc.date.accessioned2009-05-21T03:32:42Z
dc.date.available2009-05-21T03:32:42Z
dc.date.copyright2009en_US
dc.date.issued2009
dc.identifier.urihttp://hdl.handle.net/10356/16105
dc.description.abstractDesign of the different wing designs which is fixed onto the flapping mechanism known as Ornithopter. Apparatus such as whirling arm test rig and the wind tunnel are used to test and evaluate the flight performance and characteristic of the different wing designs used onto the flapping mechanism.en_US
dc.format.extent138 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineering::Aeronautical engineering::Aircraften_US
dc.titleTesting and evaluation of flapping wing mechanismen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorLow Kin Huat (MAE)en_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeMECHANICAL ENGINEERINGen_US
dc.contributor.organizationDefence Science Organisation (DSO)en_US
dc.contributor.researchFacility for Analysis, Characterisation, Testing and Simulationen_US


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