ANALISIS KEKUATAN WING PESAWAT UAV MACM 01 BERMATERIAL KOMPOSIT DENGAN FIBER CLOTH TERHADAP BEBAN BENDING

SUBARKAH MARPAUNG, IMAM (2018) ANALISIS KEKUATAN WING PESAWAT UAV MACM 01 BERMATERIAL KOMPOSIT DENGAN FIBER CLOTH TERHADAP BEBAN BENDING. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

Composite is a macroscopic combination of materials, so that mixed materials can still be seen with the naked eye. By merging macroscopically the superior properties of each material can be utilized. Fiber Cloth is a material that looks like a thin cloth. The purpose of this final project is to know the manufacturing process wing UAV MACM 01 using hand lay-up method, to know the total bending load that can be withheld by wing UAV MACM 01, knowing bending voltage that can be withheld by wing UAV MACM 01, and knowing the failure of the wing structure due to the effect of bending loads held by wing UAV MACM 01. The research method used here is the experimental method. Research starts from the wing manufacturing process, bending testing, and the last is the calculation process. The maximum bending load that can be resisted by wing UAV MACM 01 is 84.5 N. The bending voltage that can be withheld by wing MACM 01 is 9,8024 Pa.

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