Study of flutter on a composite UAV wing
A study of flutter of the VAV composite wing has been done by considering the aeroelasticity phenomenon which involves the dynamic instability of a structure which able to lead a catastrophic failure. To prevent any failure, various design effects and materials parameters of the wing structure for a...
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Format: | Thesis |
Language: | English |
Published: |
2017
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Online Access: | http://eprints.utm.my/id/eprint/78962/1/NurulZubaidahZakiMFKM2017.pdf http://eprints.utm.my/id/eprint/78962/ http://dms.library.utm.my:8080/vital/access/manager/Repository/vital:108174 |
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Institution: | Universiti Teknologi Malaysia |
Language: | English |